diff --git a/.gitignore b/.gitignore
new file mode 100644
index 0000000000000000000000000000000000000000..762762f2ef2a1184f3c98901a2ea745f0ebace61
--- /dev/null
+++ b/.gitignore
@@ -0,0 +1,7 @@
+__pycache__/
+*.py[cod]
+.venv/
+.cache/
+outputs/
+.env
+.env.*
diff --git a/LICENSE b/LICENSE
new file mode 100644
index 0000000000000000000000000000000000000000..d645695673349e3947e8e5ae42332d0ac3164cd7
--- /dev/null
+++ b/LICENSE
@@ -0,0 +1,202 @@
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diff --git a/LICENSE.md b/LICENSE.md
new file mode 100644
index 0000000000000000000000000000000000000000..d682a0a2c5fee18d63d5c09604cac57660ab3867
--- /dev/null
+++ b/LICENSE.md
@@ -0,0 +1,12 @@
+# Component licenses and attribution
+
+This collection contains original and adapted material. The Hub uses `license: other` with this file as its license entry point because no single license label describes every component.
+
+| Component | Retained terms / notice |
+| --- | --- |
+| EasyFoam project code and original project material | Existing project Apache-2.0 license in `LICENSE`, subject to third-party exceptions |
+| Inherited FoamBench Basic/Advanced task content | Upstream BSD-3-Clause notice in `LICENSES/FoamBench-BSD-3-Clause.txt`; retain applicable OpenFOAM/other embedded notices |
+| OpenFOAM tutorial-derived case content and geometry | Existing GPL-3.0-or-later notices and `LICENSES/GPL-3.txt`; see `benchmarks/assets/README.md` and `manifest.json` |
+| Generated task catalogs | Projections of the corresponding task records; preserve their source attribution and applicable terms |
+
+The packaging does not relicense upstream content or override embedded notices. Scientific authorship of the evaluation/reference data and original ExtFoamBench task design is distinguished from upstream ownership in `docs/PROVENANCE.md`. No new CC-BY, CC0 or other blanket grant is introduced by this release.
diff --git a/LICENSES/FoamBench-BSD-3-Clause.txt b/LICENSES/FoamBench-BSD-3-Clause.txt
new file mode 100644
index 0000000000000000000000000000000000000000..6347c8e0951c147d7fd36770691cd03c506227cb
--- /dev/null
+++ b/LICENSES/FoamBench-BSD-3-Clause.txt
@@ -0,0 +1,28 @@
+BSD 3-Clause License
+
+Copyright (c) 2025, Alliance for Sustainable Energy, LLC and Rensselaer Polytechnic Institute
+
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diff --git a/LICENSES/GPL-3.txt b/LICENSES/GPL-3.txt
new file mode 100644
index 0000000000000000000000000000000000000000..94a9ed024d3859793618152ea559a168bbcbb5e2
--- /dev/null
+++ b/LICENSES/GPL-3.txt
@@ -0,0 +1,674 @@
+                    GNU GENERAL PUBLIC LICENSE
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diff --git a/README.md b/README.md
new file mode 100644
index 0000000000000000000000000000000000000000..f4316fbde5b257f4f7ef8e647d6f952e5f7f5f84
--- /dev/null
+++ b/README.md
@@ -0,0 +1,170 @@
+---
+pretty_name: ExtFoamBench — CFD Tasks, Evaluation Protocols and Offline Reference Data
+language:
+- en
+license: other
+license_name: easyfoam-benchmarks-component-licenses
+license_link: LICENSE.md
+size_categories:
+- n<1K
+tags:
+- benchmark
+- computational-fluid-dynamics
+- openfoam
+- scientific-computing
+- agents
+- physics
+- evaluation
+- reference-data
+configs:
+- config_name: extended
+  default: true
+  data_files:
+  - split: test
+    path: data/extended.jsonl
+- config_name: basic
+  data_files:
+  - split: test
+    path: data/basic.jsonl
+- config_name: advanced
+  data_files:
+  - split: test
+    path: data/advanced.jsonl
+- config_name: all
+  data_files:
+  - split: test
+    path:
+    - data/extended.jsonl
+    - data/basic.jsonl
+    - data/advanced.jsonl
+---
+
+# ExtFoamBench
+
+**100 new CFD tasks, task-specific QoI acceptance rules, and offline reference data for evaluating OpenFOAM agents.**
+
+This release accompanies [EasyFoam: Skill-Oriented OpenFOAM Agents with Evidence-Driven Evolution](https://openreview.net/forum?id=GhQ5YmhU8B). It brings together three research contributions: the **ExtFoamBench task dataset**, the **execution / numerical / physical acceptance evaluation framework**, and **offline reference simulations summarized as QoIs and numerical diagnostics**.
+
+The EasyFoam Skill library is available separately on [GitHub](https://github.com/CAS-CLab/EasyFoam). Installing that library does not require downloading this dataset. This dataset includes an offline evaluator; using it does not require installing the EasyFoam agent or providing a model API key.
+
+## Contributions and attribution
+
+| Component | Task count | Task origin | Contribution in this release |
+| --- | ---: | --- | --- |
+| **ExtFoamBench / Extended** | **100** | New task suite developed by the EasyFoam authors, using attributed CFD source cases and geometry | New tasks, task-specific evaluation rules, and offline reference data |
+| FoamBench Basic | 110 | Existing [FoamBench / CFDLLMBench](https://github.com/NLR-Theseus/cfdllmbench), adapted for OpenFOAM Foundation 13 | Evaluation rules and offline reference data developed/generated by the EasyFoam authors |
+| FoamBench Advanced | 16 | Existing FoamBench / CFDLLMBench, adapted for OpenFOAM Foundation 13 | Evaluation rules and offline reference data developed/generated by the EasyFoam authors |
+
+**The 126 Basic/Advanced tasks are not claimed as an original EasyFoam dataset.** They are included for compatibility with the evaluation suite. The EasyFoam authors' evaluation and offline-reference contributions cover all **226** tasks. Existing geometry, OpenFOAM tutorials, and upstream benchmark materials retain their provenance and licenses.
+
+The default Hub configuration, `extended`, shows only the 100 ExtFoamBench tasks. `basic` and `advanced` expose inherited tasks separately. `all` combines the 226 evaluation tasks. The `test` split name means benchmark evaluation tasks; it does **not** describe the historical held-out split used in the EasyFoam skill-evolution experiments.
+
+## ExtFoamBench coverage
+
+Each of the ten families contains ten tasks: a baseline and nine variants.
+
+| Family | Physical setting |
+| --- | --- |
+| `yPlusVerification` | Near-wall resolution and wall-law verification |
+| `risingBubble` | Buoyancy-driven two-phase bubble motion |
+| `supersonicCrossJet` | Supersonic cross-flow / jet interaction |
+| `nozzleCDV` | Compressible converging-diverging nozzle flow |
+| `MRF_stirredReactor` | Rotating stirred-reactor flow |
+| `ERCOFTA_pump` | Rotating-pump pressure and flow response |
+| `compressibleBubbleCollapse` | Compressible bubble-collapse dynamics |
+| `aerofoilNACA0012` | Airfoil aerodynamic response |
+| `drivaerFastback` | Vehicle external aerodynamics |
+| `riemann2D` | Two-dimensional compressible Riemann flow |
+
+Variants cover operating conditions and boundary conditions, geometry and mesh, physics and closure models, solver/numerical settings, and study/workflow requirements. Some tasks require multiple runs, comparisons, parallel execution, or restart workflows.
+
+## What is downloaded?
+
+| Location | Contents |
+| --- | --- |
+| `data/*.jsonl` | Hub-readable task catalog: identifiers, original requirements, origin, and permitted geometry identifiers |
+| `benchmarks/FoamBench_*_fixed*.json` | Reference case input dictionaries, including OpenFOAM files and any reference subcases |
+| `benchmarks/FoamBench_*_reference_qois.json` | Offline reference QoIs, principal metrics, and acceptance tolerances for each track |
+| `benchmarks/FoamBench_extended_*measurement_specs.json` | Per-task measurement definitions for ExtFoamBench |
+| `benchmarks/FoamBench_extended_*qoi_design.json` | Family/branch QoI design and principal-versus-diagnostic roles |
+| `benchmarks/FoamBench_extended_*evidence_contract.v1.json` | Evidence format and discovery contract |
+| `benchmarks/reference_statistics/` | Parsed reference residual, Courant, continuity, and related numerical diagnostics |
+| `benchmarks/assets/` | Seven geometry assets, original source locations, and SHA-256 checksums |
+| `benchmarks/evaluation/`, `schemas/` | Offline evaluation implementation and validation schemas |
+| `benchmarks/scripts/` | Reference materialization, extraction, comparison, and asset checking utilities |
+| `metadata/` | Version, family coverage, missing-data inventory, and source checksums |
+| `docs/` | Data format, evaluation, provenance, and release notes |
+
+Reference data are **simulation-derived computational references**, with the assumptions and limits of their configurations. Raw solution fields, raw reference logs, historical agent rollouts, and paper-result archives are not included in this release. No historical train/validation/test split is inferred or invented.
+
+## Quick start: inspect a task locally
+
+From the downloaded repository root, using Python 3.11 or 3.12:
+
+```bash
+python examples/inspect_task.py --track extended --case-id nozzleCDV/1
+python scripts/verify_release.py
+```
+
+Both commands use the Python standard library and do not run a model or a CFD solver. The inspection command shows the task plus the associated measurement and reference-metric summary. Its output is intended for a human or evaluator, not as an agent prompt.
+
+For the Hub task catalog, install `datasets` in a separate environment from the pinned evaluator dependencies, and use:
+
+```python
+from datasets import load_dataset
+
+tasks = load_dataset("Eurus132/ExtFoamBench", "extended", split="test")
+print(len(tasks))  # 100
+print(tasks[0]["usr_requirement"])
+```
+
+The task catalog excludes reference input files and reference values. Load/download the full repository if you need the evaluator and reference data; `load_dataset` loads only the selected task table. Pin the repository revision when reporting experiments.
+
+## Quick start: validate the evaluator inputs
+
+```bash
+python -m pip install -r requirements.txt
+python -m benchmarks.evaluation validate-profile --profile benchmarks/evaluation/profiles/extended.json
+python -m benchmarks.evaluation validate-profile --profile benchmarks/evaluation/profiles/basic.json
+python -m benchmarks.evaluation validate-profile --profile benchmarks/evaluation/profiles/advanced.json
+python benchmarks/scripts/validate_benchmark_assets.py --benchmark benchmarks/FoamBench_extended_openfoam13_fixed.json --manifest benchmarks/assets/manifest.json
+```
+
+These checks require no OpenFOAM installation. Materialize one **reference input case** without solving it:
+
+```bash
+python benchmarks/scripts/materialize_benchmark.py --benchmark benchmarks/FoamBench_basic_openfoam13_fixed_final.json --case-id Cavity/1 --output-root outputs/reference-input
+```
+
+Actual CFD simulation requires **OpenFOAM Foundation 13** and the appropriate system tools. This release does not launch an agent. The offline evaluator consumes existing run artifacts; some derived measurements require native OpenFOAM tools. See [Evaluation](docs/EVALUATION.md) before enabling preparation or mesh auditing.
+
+## Evaluation: execution, numerics, and physics
+
+The framework measures whether a task completes (**E**), satisfies applicable numerical checks (**N**), and satisfies every mandatory task-specific physical/QoI criterion (**Q**). It reports execution completion rate (**ECR**) and joint task acceptance rate (**TAR**):
+
+```text
+ECR = count(E passes) / number of assigned tasks
+TAR = count(E and N and Q all pass) / number of assigned tasks
+```
+
+A high ECR alone does not establish physically acceptable task completion. Measurements can be scalars, spatial profiles, time histories, events, or branch-dependent responses. The supplied contracts fix extraction semantics, tolerances, missing-evidence behavior, and aggregation. Optional diagnostic scores and continuous quality values are not substitutes for mandatory acceptance checks or TAR.
+
+See [Evaluation](docs/EVALUATION.md) for the implementation fields, [Data format](docs/DATA_FORMAT.md) for file relationships, and [release notes](docs/RELEASE_NOTES.md) for current protocol boundaries.
+
+## Reference visibility and intended use
+
+This is a public research dataset and evaluation resource. Give a solving agent only the selected task requirements, allowed assets, and explicitly task-visible measurement instructions. Keep reference inputs, reference values, and evaluator files outside its accessible workspace. A working-directory setting alone is not read-access isolation.
+
+The benchmark supports comparative research under its declared contracts. Passing it is not a general certification of physical validity or engineering suitability. Researchers should report software/data revisions, model and runtime settings, task membership, and any changed acceptance rules.
+
+## Data completeness and versioning
+
+All 226 tasks have reference-QoI case entries. Parsed numerical reference statistics are nonempty for **215 of 226** tasks. They are unavailable for `nozzleCDV/4` and all ten `riemann2D` tasks in the Extended track; missing statistics are recorded explicitly in [coverage.json](metadata/coverage.json), not filled with synthetic values. Case-entry presence is not a claim that every optional diagnostic or conditional QoI is available.
+
+Release `1.0.0` packages the supplied data and scorer without changing their numerical contents. Embedded schema versions and the Extended contract's `provisional` tolerance status are retained. This package is not a certification that all current defaults reproduce every historical table in the manuscript. Changes to tasks, reference values, extraction, or scoring require a new release. See [release notes](docs/RELEASE_NOTES.md).
+
+## Attribution and licenses
+
+Use of ExtFoamBench tasks or the EasyFoam evaluation/reference resources should cite the [EasyFoam paper](https://openreview.net/forum?id=GhQ5YmhU8B). Use of Basic/Advanced should also credit the [upstream FoamBench work](https://github.com/NLR-Theseus/cfdllmbench). Dataset originality and reuse permissions are described separately in [Provenance](docs/PROVENANCE.md) and [component licenses](LICENSE.md).
+
+This is a mixed-origin collection. The repository does not apply a new blanket license that overrides upstream terms. Apache-2.0 project terms, the FoamBench BSD-3-Clause notice, and OpenFOAM GPL notices are retained in `LICENSE` and `LICENSES/`.
diff --git a/SHA256SUMS b/SHA256SUMS
new file mode 100644
index 0000000000000000000000000000000000000000..9efbc54333445d72d65ea3b145b24efdda28e99b
--- /dev/null
+++ b/SHA256SUMS
@@ -0,0 +1,102 @@
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diff --git a/VERSION b/VERSION
new file mode 100644
index 0000000000000000000000000000000000000000..3eefcb9dd5b38e2c1dc061052455dd97bcd51e6c
--- /dev/null
+++ b/VERSION
@@ -0,0 +1 @@
+1.0.0
diff --git a/benchmarks/FoamBench_advanced_openfoam13_fixed_final.json b/benchmarks/FoamBench_advanced_openfoam13_fixed_final.json
new file mode 100644
index 0000000000000000000000000000000000000000..d209b81f6bf17c3d618615edd47e53092582d9e4
--- /dev/null
+++ b/benchmarks/FoamBench_advanced_openfoam13_fixed_final.json
@@ -0,0 +1,285 @@
+{
+  "Double_Square_SA": {
+    "usr_requirement": "Perform an incompressible turbulent flow simulation over two square obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 5 in x direction and 0 to 2.5 in y direction and -0.5 to 0.5 in z direction. One of the square obstacle is of size  1 unit x 1 unit x 1 unit centered at 1.5 x 1.25 x 0.0 and the other square obstacle is of size 1 unit x 1 unit x 1 unit centered at 3.5 x 1.25 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 5000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        nuTilda         0.4;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         5;\ndeltaT          0.01;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.5;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxDeltaT       0.05;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 6;\n\nmethod          hierarchical;\n\ncoeffs\n{\n    n           (3 2 1);\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss upwind;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n// bottom layer (z = -0.5)\n    (0.0 0.0 -0.5) //  0\n    (1.0 0.0 -0.5) //  1\n    (2.0 0.0 -0.5) //  2\n    (3.0 0.0 -0.5) //  3\n    (4.0 0.0 -0.5) //  4\n    (5.0 0.0 -0.5) //  5\n\n    (0.0 0.75 -0.5) //  6\n    (1.0 0.75 -0.5) //  7\n    (2.0 0.75 -0.5) //  8\n    (3.0 0.75 -0.5) //  9\n    (4.0 0.75 -0.5) // 10\n    (5.0 0.75 -0.5) // 11\n\n    (0.0 1.75 -0.5) // 12\n    (1.0 1.75 -0.5) // 13\n    (2.0 1.75 -0.5) // 14\n    (3.0 1.75 -0.5) // 15\n    (4.0 1.75 -0.5) // 16\n    (5.0 1.75 -0.5) // 17\n\n    (0.0 2.5  -0.5) // 18\n    (1.0 2.5  -0.5) // 19\n    (2.0 2.5  -0.5) // 20\n    (3.0 2.5  -0.5) // 21\n    (4.0 2.5  -0.5) // 22\n    (5.0 2.5  -0.5) // 23\n\n// top layer (z = +0.5)\n    (0.0 0.0 0.5) // 24\n    (1.0 0.0 0.5) // 25\n    (2.0 0.0 0.5) // 26\n    (3.0 0.0 0.5) // 27\n    (4.0 0.0 0.5) // 28\n    (5.0 0.0 0.5) // 29\n\n    (0.0 0.75 0.5) // 30\n    (1.0 0.75 0.5) // 31\n    (2.0 0.75 0.5) // 32\n    (3.0 0.75 0.5) // 33\n    (4.0 0.75 0.5) // 34\n    (5.0 0.75 0.5) // 35\n\n    (0.0 1.75 0.5) // 36\n    (1.0 1.75 0.5) // 37\n    (2.0 1.75 0.5) // 38\n    (3.0 1.75 0.5) // 39\n    (4.0 1.75 0.5) // 40\n    (5.0 1.75 0.5) // 41\n\n    (0.0 2.5  0.5) // 42\n    (1.0 2.5  0.5) // 43\n    (2.0 2.5  0.5) // 44\n    (3.0 2.5  0.5) // 45\n    (4.0 2.5  0.5) // 46\n    (5.0 2.5  0.5) // 47\n);\n\nblocks\n(\n// bottom strip y ∈ [0,0.75]\n    hex ( 0  1  7  6 24 25 31 30) (20 15 1) simpleGrading (1 1 1)\n    hex ( 1  2  8  7 25 26 32 31) (20 15 1) simpleGrading (1 1 1)\n    hex ( 2  3  9  8 26 27 33 32) (20 15 1) simpleGrading (1 1 1)\n    hex ( 3  4 10  9 27 28 34 33) (20 15 1) simpleGrading (1 1 1)\n    hex ( 4  5 11 10 28 29 35 34) (20 15 1) simpleGrading (1 1 1)\n\n// middle strip y ∈ [0.75,1.75], skipping posts at ix=1 & ix=3\n    hex ( 6  7 13 12 30 31 37 36) (20 20 1) simpleGrading (1 1 1)\n    hex ( 8  9 15 14 32 33 39 38) (20 20 1) simpleGrading (1 1 1)\n    hex (10 11 17 16 34 35 41 40) (20 20 1) simpleGrading (1 1 1)\n\n// top strip y ∈ [1.75,2.5]\n    hex (12 13 19 18 36 37 43 42) (20 15 1) simpleGrading (1 1 1)\n    hex (13 14 20 19 37 38 44 43) (20 15 1) simpleGrading (1 1 1)\n    hex (14 15 21 20 38 39 45 44) (20 15 1) simpleGrading (1 1 1)\n    hex (15 16 22 21 39 40 46 45) (20 15 1) simpleGrading (1 1 1)\n    hex (16 17 23 22 40 41 47 46) (20 15 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 30 24)\n            (6 12 36 30)\n            (12 18 42 36)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (5 11 35 29)\n            (11 17 41 35)\n            (17 23 47 41)\n        );\n    }\n    bottomWall\n    {\n        type wall;\n        faces\n        (\n            (0 1 25 24)\n            (1 2 26 25)\n            (2 3 27 26)\n            (3 4 28 27)\n            (4 5 29 28)\n        );\n    }\n    topWall\n    {\n        type wall;\n        faces\n        (\n            (18 19 43 42)\n            (19 20 44 43)\n            (20 21 45 44)\n            (21 22 46 45)\n            (22 23 47 46)\n        );\n    }\n    posts\n    {\n        type wall;\n        faces\n        (\n            // left square post at ix=1,iy=1\n            (7 13 37 31)\n            (8 14 38 32)\n            (7 8 32 31)\n            (13 14 38 37)\n            // right square post at ix=3,iy=1\n            (9 15 39 33)\n            (10 16 40 34)\n            (9 10 34 33)\n            (15 16 40 39)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            // z = -0.5 faces (one per block, bottom-layer)\n            (0 1 7 6)\n            (1 2 8 7)\n            (2 3 9 8)\n            (3 4 10 9)\n            (4 5 11 10)\n            (6 7 13 12)\n            (8 9 15 14)\n            (10 11 17 16)\n            (12 13 19 18)\n            (13 14 20 19)\n            (14 15 21 20)\n            (15 16 22 21)\n            (16 17 23 22)\n            // z = +0.5 faces (top-layer)\n            (24 25 31 30)\n            (25 26 32 31)\n            (26 27 33 32)\n            (27 28 34 33)\n            (28 29 35 34)\n            (30 31 37 36)\n            (32 33 39 38)\n            (34 35 41 40)\n            (36 37 43 42)\n            (37 38 44 43)\n            (38 39 45 44)\n            (39 40 46 45)\n            (40 41 47 46)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 2e-7;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2e-7;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }    bottomWall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    topWall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    posts\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    bottomWall\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    topWall\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    posts\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    bottomWall\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    topWall\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    posts\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    bottomWall\n    {\n        type            calculated;\n        value           uniform 0;\n    }    topWall\n    {\n        type            calculated;\n        value           uniform 0;\n    }    posts\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-06;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n"
+  },
+  "wedge_SA": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge using. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 5 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The Pr for the mixture is 1. Use rhoCentralFoam solver. Use SpalartAllmaras turbulence model. The wedge surface is a slip boundary. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"(U|h|e|T|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"(U|h|e|T|nuTilda).*Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          shockFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.2;\ndeltaT          0.0001;\n\nwriteControl    runTime;\nwriteInterval   0.02;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1e-06;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n    div(phi,nuTilda) bounded Gauss upwind;\n    div(phi,U)      bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n    laplacian(nuEff,U) Gauss linear corrected;\n    laplacian(1,nuTilda) Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)   vanLeerV;\n    reconstruct(T)   vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1e-5;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 1e-5;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    top\n    {\n        type            symmetryPlane;\n    }    obstacle\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    top\n    {\n        type            symmetryPlane;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (5 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    top\n    {\n        type            symmetryPlane;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    bottom\n    {\n        type            symmetryPlane;   // Correct boundary condition\n    }\n    top\n    {\n        type            symmetryPlane;   // Correct boundary condition\n    }    obstacle\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    top\n    {\n        type            symmetryPlane;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    top\n    {\n        type            symmetryPlane;\n    }\n    obstacle\n    {\n        type            calculated;     // ✅ Replaced alphatWallFunction with calculated\n        value           uniform 0;      // Placeholder required even if not directly used\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0.01;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder_LES": {
+    "usr_requirement": "do a offsetcylinder simulation using Large eddy simulation with dynamic kinetic energy equation model. Use PIMPLE algorithm. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.5;\ndeltaT          0.0025;\n\nwriteControl    runTime;\nwriteInterval   0.05;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    right\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    down\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    up\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    down\n    {\n        type            zeroGradient;\n    }\n    up\n    {\n        type            zeroGradient;\n    }\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform 2e-05;\n    }\n    right\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    down\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    up\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n    right\n    {\n        type            zeroGradient;\n    }\n    down\n    {\n        type            noSlip;\n    }\n    up\n    {\n        type            noSlip;\n    }\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n    right\n    {\n        type            zeroGradient;\n    }\n    down\n    {\n        type            zeroGradient;\n    }\n    up\n    {\n        type            zeroGradient;\n    }\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  LES;\n\nLES\n{\n    model           dynamicKEqn;\n    delta           cubeRootVol;\n    filter          simple;\n    turbulence      on;\n    printCoeffs     on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 0.01;\n\n// ************************************************************************* //\n"
+  },
+  "Diamond_Obstacle_KOMEGASST": {
+    "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D diamond obstacle using the k-Omega SST RANS turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The diamond obstacle is a square rotated by 45 degrees with diagonal length of 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to diamond. Use sufficient grid points to discretize the domain and dont use more than 10000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The diamond obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        k               0.5;\n        omega           0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         5;\ndeltaT          0.01;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.5;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.2;\nmaxDeltaT       0.05;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 6;\n\nmethod          hierarchical;\n\ncoeffs\n{\n    n           (3 2 1);\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss upwind;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss upwind;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nscale   1;\n\nvertices\n(\n    (0    0   -0.5) //  0\n    (2    0   -0.5) //  1\n    (3    0   -0.5) //  2\n    (15   0   -0.5) //  3\n    (15   2   -0.5) //  4\n    (15   3   -0.5) //  5\n    (15   5   -0.5) //  6\n    (3    5   -0.5) //  7\n    (2    5   -0.5) //  8\n    (0    5   -0.5) //  9\n    (0    3   -0.5) // 10\n    (0    2   -0.5) // 11\n\n    // Diamond hole on bottom face:\n    (2.5  2   -0.5) // 12 — midpoint of 11–13\n    (3    2.5 -0.5) // 13 — midpoint of 13–14\n    (2.5  3   -0.5) // 14 — midpoint of 14–15\n    (2    2.5 -0.5) // 15 — midpoint of 12–11\n\n    (0    0    0.5) // 16\n    (2    0    0.5) // 17\n    (3    0    0.5) // 18\n    (15   0    0.5) // 19\n    (15   2    0.5) // 20\n    (15   3    0.5) // 21\n    (15   5    0.5) // 22\n    (3    5    0.5) // 23\n    (2    5    0.5) // 24\n    (0    5    0.5) // 25\n    (0    3    0.5) // 26\n    (0    2    0.5) // 27\n\n    // Diamond hole on top face:\n    (2.5  2    0.5) // 28\n    (3    2.5  0.5) // 29\n    (2.5  3    0.5) // 30\n    (2    2.5  0.5) // 31\n);\n\nblocks\n(\n    hex (0  1 12 11 16 17 28 27) (50 25 1) simpleGrading (1 1 1)\n    hex (11 12 15 10 27 28 31 26) (50 25 1) simpleGrading (1 1 1)\n    hex (10 15  8  9 26 31 24 25) (50 25 1) simpleGrading (1 1 1)\n    hex (15 14  7  8 31 30 23 24) (50 25 1) simpleGrading (1 1 1)\n    hex (1  2 13 12 17 18 29 28) (50 25 1) simpleGrading (1 1 1)\n    hex (14  5  6  7 30 21 22 23) (50 25 1) simpleGrading (4 1 1)\n    hex (13  4  5 14 29 20 21 30) (50 25 1) simpleGrading (4 1 1)\n    hex (2   3  4 13 18 19 20 29) (50 25 1) simpleGrading (4 1 1)\n);\n\nedges\n(\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3  4  20 19)\n            (4  5  21 20)\n            (5  6  22 21)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (11 0  16 27)\n            (10 11 27 26)\n            (9  10 26 25)\n        );\n    }\n\n    wall1\n    {\n        type wall;\n        faces\n        (\n            (6  7  23 22)\n            (7  8  24 23)\n            (8  9  25 24)\n        );\n    }\n\n    wall2\n    {\n        type wall;\n        faces\n        (\n            (0  1  17 16)\n            (1  2  18 17)\n            (2  3  19 18)\n        );\n    }\n\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (15 12 28 31)\n            (14 15 31 30)\n            (12 13 29 28)\n            (13 14 30 29)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    outlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    inlet\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall2\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    cylinder\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-4;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1e-4;\n    }\n    wall1\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n    wall2\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n    cylinder\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1 0 0);\n\nboundaryField\n{\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    wall2\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-6;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    wall1\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n    wall2\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n    cylinder\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 50;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthFrequencyInlet;\n        mixingLength    1.2;\n        value           uniform 50;\n    }\n    wall1\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n    wall2\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n    cylinder\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-06;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n"
+  },
+  "Cavity_SA": {
+    "usr_requirement": "do an incompressible of lid driven cavity flow using pisoFoam solver and SpalartAllmaras turbulence model. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         10;\ndeltaT          0.005;\n\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    movingWall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    fixedWalls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n    fixedWalls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    movingWall\n    {\n        type            calculated;\n        value           uniform 0;\n    }    fixedWalls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 1e-05;\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D_SA": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM, employing a compressible flow solver for detailed combustion modeling. Use SpalartAllmaras turbulence model. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with foamRun -solver multicomponentFluid, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    rho\n    {\n        solver          diagonal;\n    }\n\n    rhoFinal\n    {\n        $rho;\n    }\n\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|h|e|T|k|epsilon|omega|nuTilda|Yi|CH4|O2|N2|CO2|H2O|Ydefault)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|e|T|k|epsilon|omega|nuTilda|Yi|CH4|O2|N2|CO2|H2O|Ydefault)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"            0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          multicomponentFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.5;\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.05;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.4;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,h)      Gauss limitedLinear 1;\n    div(phi,e)      Gauss limitedLinear 1;\n    div(phi,T)      Gauss limitedLinear 1;\n    div(phi,Yi)     Gauss limitedLinear 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1e-5;   // Small non-zero value at inlet\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 1e-5;   // Small non-zero value at inlet\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 30000;\n\nboundaryField\n{\n    fuel\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.000504;\n        phi             phi;\n        k               k;\n        value           uniform 1;\n    }\n    air\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.019677;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.1 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    air\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    outlet\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      thermo.compressibleGas;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      reactions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock_LES": {
+    "usr_requirement": "do a 2D oblique shock wave LES simulation (Smagorinsky model) using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"(U|h|e|T|k|nut|alphat).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"(U|h|e|T|k|nut|alphat).*Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          shockFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         10;\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\nwriteInterval   1;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.2;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)   vanLeerV;\n    reconstruct(T)   vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  LES;\n\nLES\n{\n    model           Smagorinsky;\n    turbulence      on;\n    printCoeffs     on;\n\ndelta           cubeRootVol;\n\nSmagorinskyCoeffs\n{\n    Cs          0.17;\n}\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity_geometry_1": {
+    "usr_requirement": "do an incompressible of lid driven cavity flow using pisoFoam solver and SpalartAllmaras turbulence model. The cavity is a square with dimensions normalized to 2 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 40X40 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         10;\ndeltaT          0.005;\n\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (2 0 0)\n    (2 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (2 0 0.1)\n    (2 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (40 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    movingWall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    fixedWalls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n    fixedWalls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    movingWall\n    {\n        type            calculated;\n        value           uniform 0;\n    }    fixedWalls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 1e-05;\n\n// ************************************************************************* //\n"
+  },
+  "Diamond_Obstacle_SA": {
+    "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D diamond obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The diamond obstacle is a square rotated by 45 degrees with diagonal length of 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to diamond. Use sufficient grid points to discretize the domain and dont use more than 10000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The diamond obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         5;\ndeltaT          0.5;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.5;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 6;\n\nmethod          hierarchical;\n\ncoeffs\n{\n    n           (3 2 1);\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nscale   1;\n\nvertices\n(\n    (0    0   -0.5) //  0\n    (2    0   -0.5) //  1\n    (3    0   -0.5) //  2\n    (15   0   -0.5) //  3\n    (15   2   -0.5) //  4\n    (15   3   -0.5) //  5\n    (15   5   -0.5) //  6\n    (3    5   -0.5) //  7\n    (2    5   -0.5) //  8\n    (0    5   -0.5) //  9\n    (0    3   -0.5) // 10\n    (0    2   -0.5) // 11\n\n    // Diamond hole on bottom face:\n    (2.5  2   -0.5) // 12 — midpoint of 11–13\n    (3    2.5 -0.5) // 13 — midpoint of 13–14\n    (2.5  3   -0.5) // 14 — midpoint of 14–15\n    (2    2.5 -0.5) // 15 — midpoint of 12–11\n\n    (0    0    0.5) // 16\n    (2    0    0.5) // 17\n    (3    0    0.5) // 18\n    (15   0    0.5) // 19\n    (15   2    0.5) // 20\n    (15   3    0.5) // 21\n    (15   5    0.5) // 22\n    (3    5    0.5) // 23\n    (2    5    0.5) // 24\n    (0    5    0.5) // 25\n    (0    3    0.5) // 26\n    (0    2    0.5) // 27\n\n    // Diamond hole on top face:\n    (2.5  2    0.5) // 28\n    (3    2.5  0.5) // 29\n    (2.5  3    0.5) // 30\n    (2    2.5  0.5) // 31\n);\n\nblocks\n(\n    hex (0  1 12 11 16 17 28 27) (50 25 1) simpleGrading (1 1 1)\n    hex (11 12 15 10 27 28 31 26) (50 25 1) simpleGrading (1 1 1)\n    hex (10 15  8  9 26 31 24 25) (50 25 1) simpleGrading (1 1 1)\n    hex (15 14  7  8 31 30 23 24) (50 25 1) simpleGrading (1 1 1)\n    hex (1  2 13 12 17 18 29 28) (50 25 1) simpleGrading (1 1 1)\n    hex (14  5  6  7 30 21 22 23) (50 25 1) simpleGrading (4 1 1)\n    hex (13  4  5 14 29 20 21 30) (50 25 1) simpleGrading (4 1 1)\n    hex (2   3  4 13 18 19 20 29) (50 25 1) simpleGrading (4 1 1)\n);\n\nedges\n(\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3  4  20 19)\n            (4  5  21 20)\n            (5  6  22 21)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (11 0  16 27)\n            (10 11 27 26)\n            (9  10 26 25)\n        );\n    }\n\n    wall1\n    {\n        type wall;\n        faces\n        (\n            (6  7  23 22)\n            (7  8  24 23)\n            (8  9  25 24)\n        );\n    }\n\n    wall2\n    {\n        type wall;\n        faces\n        (\n            (0  1  17 16)\n            (1  2  18 17)\n            (2  3  19 18)\n        );\n    }\n\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (15 12 28 31)\n            (14 15 31 30)\n            (12 13 29 28)\n            (13 14 30 29)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-6;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1e-6;\n    }    wall1\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    wall2\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    outlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    inlet\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall2\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    cylinder\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1 0 0);\n\nboundaryField\n{\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    wall2\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 6.12e-2;\n\nboundaryField\n{    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    wall1\n    {\n        type            calculated;\n        value           uniform 0;\n    }    wall2\n    {\n        type            calculated;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-06;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D_KE": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM, employing a compressible flow solver for detailed combustion modeling. Use k-epsilon turbulence model. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with foamRun -solver multicomponentFluid, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    rho\n    {\n        solver          diagonal;\n    }\n\n    rhoFinal\n    {\n        $rho;\n    }\n\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|h|e|T|k|epsilon|omega|nuTilda|Yi|CH4|O2|N2|CO2|H2O|Ydefault)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|e|T|k|epsilon|omega|nuTilda|Yi|CH4|O2|N2|CO2|H2O|Ydefault)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"            0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          multicomponentFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.5;\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.05;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.4;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,h)      Gauss limitedLinear 1;\n    div(phi,e)      Gauss limitedLinear 1;\n    div(phi,T)      Gauss limitedLinear 1;\n    div(phi,Yi)     Gauss limitedLinear 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 30000;\n\nboundaryField\n{\n    fuel\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.000504;\n        phi             phi;\n        k               k;\n        value           uniform 1;\n    }\n    air\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.019677;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 30;\n\nboundaryField\n{\n    fuel\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.0458;\n        value           uniform 1;\n    }\n    air\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.0471;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.1 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    air\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    outlet\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      thermo.compressibleGas;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      reactions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "Rectangular_Obstacle_SA": {
+    "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D rectangular obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The rectangular obstacle is of size  1 unit x 1 unit x 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 60000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        nuTilda         0.4;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         5;\ndeltaT          0.01;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.5;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.2;\nmaxDeltaT       0.05;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 6;\n\nmethod          hierarchical;\n\ncoeffs\n{\n    n           (3 2 1);\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss upwind;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nscale   1;\n\nvertices\n(\n(0 0 -0.5) //0\n(2 0 -0.5) //1\n(3 0 -0.5) //2\n(15 0 -0.5) //3\n(15 2 -0.5) //4\n(15 3 -0.5) //5\n(15 5 -0.5) //6\n(3 5 -0.5) //7\n(2 5 -0.5) //8\n(0 5 -0.5) //9\n(0 3 -0.5) //10\n(0 2 -0.5) //11\n(2 2 -0.5) //12\n(3 2 -0.5) //13\n(3 3 -0.5) //14\n(2 3 -0.5) //15\n\n(0 0 0.5) //16\n(2 0 0.5) //17\n(3 0 0.5) //18\n(15 0 0.5) //19\n(15 2 0.5) //20\n(15 3 0.5) //21\n(15 5 0.5) //22\n(3 5 0.5) //23\n(2 5 0.5) //24\n(0 5 0.5) //25\n(0 3 0.5) //26\n(0 2 0.5) //27\n(2 2 0.5) //28\n(3 2 0.5) //29\n(3 3 0.5) //30\n(2 3 0.5) //31\n);\n\nblocks\n(\nhex (0 1 12 11 16 17 28 27) (100 50 1) simpleGrading (1 1 1)\nhex (11 12 15 10 27 28 31 26) (100 50 1) simpleGrading (1 1 1)\nhex (10 15 8 9 26 31 24 25) (100 50 1) simpleGrading (1 1 1)\nhex (15 14 7 8 31 30 23 24) (100 50 1) simpleGrading (1 1 1)\nhex (1 2 13 12 17 18 29 28) (100 50 1) simpleGrading (1 1 1)\nhex (14 5 6 7 30 21 22 23) (200 50 1) simpleGrading (4 1 1)\nhex (13 4 5 14 29 20 21 30) (200 50 1) simpleGrading (4 1 1)\nhex (2 3 4 13 18 19 20 29) (200 50 1) simpleGrading (4 1 1)\n);\n\nedges\n(\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\noutlet\n{\ntype patch;\nfaces\n(\n(3 4 20 19)\n(4 5 21 20)\n(5 6 22 21)\n);\n}\n\ninlet\n{\ntype patch;\nfaces\n(\n(11 0 16 27)\n(10 11 27 26)\n(9 10 26 25)\n);\n}\n\nwall1\n{\ntype wall;\nfaces\n(\n(6 7 23 22)\n(7 8 24 23)\n(8 9 25 24)\n);\n}\n\nwall2\n{\ntype wall;\nfaces\n(\n(0 1 17 16)\n(1 2 18 17)\n(2 3 19 18)\n\n);\n}\n\ncylinder\n{\ntype wall;\nfaces\n(\n(15 12 28 31)\n(14 15 31 30)\n(12 13 29 28)\n(13 14 30 29)\n);\n}\n\n\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 2e-7;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2e-7;\n    }    wall1\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    wall2\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    outlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    inlet\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall2\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    cylinder\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1 0 0);\n\nboundaryField\n{\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    wall2\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    wall1\n    {\n        type            calculated;\n        value           uniform 0;\n    }    wall2\n    {\n        type            calculated;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-06;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n"
+  },
+  "nozzleFlow2D_SA": {
+    "usr_requirement": "do a 2D nozzle flow simulation using interfoam solver and  Spalart-Allmaras turbulence model. Use a time step of 1e-8 seconds, output results every 1e-06s. The end time is 1e-5s. seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\n\nfor i in 1 2\ndo\n    runApplication -s $i topoSet -dict topoSetDict.${i}\n    runApplication -s $i refineMesh -dict refineMeshDict -overwrite\ndone\n\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 4;\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner\n        {\n            preconditioner  GAMG;\n            tolerance       1e-05;\n            relTol          0;\n            smoother        DICGaussSeidel;\n        }\n        tolerance       1e-05;\n        relTol          0;\n        maxIter         100;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|nuTilda)Final\"\n    {\n        $U;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 1;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1e-05;\ndeltaT          1e-08;\n\nwriteControl    adjustableRunTime;\nwriteInterval   1e-06;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict.1": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict.1;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box (0 0 -2e-05) (0.0036 0.0008 4e-05);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/refineMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      refineMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nset             c0;\n\ncoordinateSystem global;\n\nglobalCoeffs\n{\n    e1              (1 0 0);\n    e2              (0 1 0);\n}\n\npatchLocalCoeffs\n{\n    patch           outside;\n    e1              (1 0 0);\n}\n\ndirections      (e1);\n\nuseHexTopology  no;\n\ngeometricCut    yes;\n\nwriteMesh       no;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                     none;\n    div(rhoPhi,U)                              Gauss linearUpwind grad(U);\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(phi,nuTilda)                           bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U)))))              Gauss linear;\n    div(((rho*nuEff)*dev2(T(grad(U)))))        Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1e-06;\n\nvertices\n(\n    (0 0 0)\n    (3000 0 0)\n    (0 100 -4.36609429085)\n    (3000 300 -13.0982828726)\n    (0 400 -17.4643771634)\n    (3000 700 -30.562660036)\n    (0 800 -34.9287543268)\n    (3000 1000 -43.6609429085)\n    (0 1600 -69.8575086536)\n    (3000 1600 -69.8575086536)\n\n    (0 100 4.36609429085)\n    (3000 300 13.0982828726)\n    (0 400 17.4643771634)\n    (3000 700 30.562660036)\n    (0 800 34.9287543268)\n    (3000 1000 43.6609429085)\n    (0 1600 69.8575086536)\n    (3000 1600 69.8575086536)\n);\n\nblocks\n(\n    hex (0 1 3 2 0 1 11 10)\n    (75 30 1)\n    edgeGrading (1 1 1 1 0.1666667 1 1 0.1666667 1 1 1 1)\n\n    hex (2 3 5 4 10 11 13 12)\n    (75 40 1)\n    edgeGrading (1 1 1 1 20 1 1 20 1 1 1 1)\n\n    hex (4 5 7 6 12 13 15 14)\n    (75 15 1)\n    simpleGrading (1.0 1.0 1.0)\n\n    hex (6 7 9 8 14 15 17 16)\n    (75 15 1)\n    simpleGrading (1.0 1.0 1.0)\n);\n\nboundary\n(\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 1 1 0)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 0 10 2)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (2 10 12 4)\n            (4 12 14 6)\n            (6 14 16 8)\n        );\n    }\n\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (8 16 17 9)\n            (7 9 17 15)\n            (5 7 15 13)\n            (3 5 13 11)\n            (1 3 11 1)\n        );\n    }\n\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 11 10)\n            (10 11 13 12)\n            (12 13 15 14)\n            (14 15 17 16)\n        );\n    }\n\n    back\n    {\n        type wedge;\n        faces\n        (\n            (0 2 3 1)\n            (2 4 5 3)\n            (4 6 7 5)\n            (6 8 9 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/topoSetDict.2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict.2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box (0 0 -2e-05) (0.0036 0.0003 2e-05);\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/alpha.fuel": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.fuel;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    atmosphere\n    {\n        type            prghTotalPressure;\n        p0              uniform 0;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1e-5;   // Small turbulence at inlet\n    }\n    walls\n    {\n        type            epsilonWallFunction;   \n        value           uniform 1e-11;\n    }\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-11;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1e-05;\n    }\n    walls\n    {\n        type kqRWallFunction;  \n        value uniform 1e-11;\n    }\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.001;\n        value           uniform 1e-11;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (460 0 0);\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-11;\n\nboundaryField\n{\n    axis\n    {\n        type            empty;\n    }    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }    atmosphere\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/data/ptrace": "",
+    "0/data/Ubulk": "",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (fuel air);\n\nsigma           0.0261;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.fuel": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.fuel;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              5.952e-06;\n\nrho             840;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              8.5e-07;\n\nrho             20;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 1e-06;\nrho             [1 -3 0 0 0 0 0] 1000;\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.fuel 0\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0 0 0) (0.5 0.5 1);\n        fieldValues\n        (\n            volScalarFieldValue alpha.fuel 1\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "Cavity_LES": {
+    "usr_requirement": "do an incompressible large eddy simulation (using dynamic kinetic energy equation model) of lid driven cavity flow using pisoFoam solver. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         10;\ndeltaT          0.005;\n\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n    fixedWalls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  LES;\n\nLES\n{\n    model           dynamicKEqn;\n    delta           cubeRootVol;\n    filter          simple;\n    turbulence      on;\n    printCoeffs     on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 1e-05;\n\n// ************************************************************************* //\n"
+  },
+  "Rectangular_Obstacle_KOMEGASST": {
+    "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D rectangular obstacle using the k-Omega SST RANS turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The rectangular obstacle is of size  1 unit x 1 unit x 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 60000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        k               0.5;\n        omega           0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         5;\ndeltaT          0.01;\n\nwriteControl    adjustableRunTime;\nwriteInterval   0.5;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.2;\nmaxDeltaT       0.05;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 6;\n\nmethod          hierarchical;\n\ncoeffs\n{\n    n           (3 2 1);\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss upwind;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss upwind;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nscale   1;\n\nvertices\n(\n(0 0 -0.5) //0\n(2 0 -0.5) //1\n(3 0 -0.5) //2\n(15 0 -0.5) //3\n(15 2 -0.5) //4\n(15 3 -0.5) //5\n(15 5 -0.5) //6\n(3 5 -0.5) //7\n(2 5 -0.5) //8\n(0 5 -0.5) //9\n(0 3 -0.5) //10\n(0 2 -0.5) //11\n(2 2 -0.5) //12\n(3 2 -0.5) //13\n(3 3 -0.5) //14\n(2 3 -0.5) //15\n\n(0 0 0.5) //16\n(2 0 0.5) //17\n(3 0 0.5) //18\n(15 0 0.5) //19\n(15 2 0.5) //20\n(15 3 0.5) //21\n(15 5 0.5) //22\n(3 5 0.5) //23\n(2 5 0.5) //24\n(0 5 0.5) //25\n(0 3 0.5) //26\n(0 2 0.5) //27\n(2 2 0.5) //28\n(3 2 0.5) //29\n(3 3 0.5) //30\n(2 3 0.5) //31\n);\n\nblocks\n(\nhex (0 1 12 11 16 17 28 27) (100 50 1) simpleGrading (1 1 1)\nhex (11 12 15 10 27 28 31 26) (100 50 1) simpleGrading (1 1 1)\nhex (10 15 8 9 26 31 24 25) (100 50 1) simpleGrading (1 1 1)\nhex (15 14 7 8 31 30 23 24) (100 50 1) simpleGrading (1 1 1)\nhex (1 2 13 12 17 18 29 28) (100 50 1) simpleGrading (1 1 1)\nhex (14 5 6 7 30 21 22 23) (200 50 1) simpleGrading (4 1 1)\nhex (13 4 5 14 29 20 21 30) (200 50 1) simpleGrading (4 1 1)\nhex (2 3 4 13 18 19 20 29) (200 50 1) simpleGrading (4 1 1)\n);\n\nedges\n(\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\noutlet\n{\ntype patch;\nfaces\n(\n(3 4 20 19)\n(4 5 21 20)\n(5 6 22 21)\n);\n}\n\ninlet\n{\ntype patch;\nfaces\n(\n(11 0 16 27)\n(10 11 27 26)\n(9 10 26 25)\n);\n}\n\nwall1\n{\ntype wall;\nfaces\n(\n(6 7 23 22)\n(7 8 24 23)\n(8 9 25 24)\n);\n}\n\nwall2\n{\ntype wall;\nfaces\n(\n(0 1 17 16)\n(1 2 18 17)\n(2 3 19 18)\n\n);\n}\n\ncylinder\n{\ntype wall;\nfaces\n(\n(15 12 28 31)\n(14 15 31 30)\n(12 13 29 28)\n(13 14 30 29)\n);\n}\n\n\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    outlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    inlet\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    wall2\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    cylinder\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-4;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1e-4;\n    }\n    wall1\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n    wall2\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n    cylinder\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-4;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1 0 0);\n\nboundaryField\n{\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           $internalField;\n    }\n    wall1\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    wall2\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    cylinder\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 1e-6;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    wall1\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n    wall2\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n    cylinder\n    {\n        type            nutkWallFunction;\n        value           uniform 1e-6;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 50;\n\nboundaryField\n{\n    outlet\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthFrequencyInlet;\n        mixingLength    1.2;\n        value           uniform 50;\n    }\n    wall1\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n    wall2\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n    cylinder\n    {\n        type            omegaWallFunction;\n        value           uniform 50;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-06;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock_KE": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use k-epsilon turbulence model. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"(U|h|e|T|k|epsilon|nut|alphat).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"(U|h|e|T|k|epsilon|nut|alphat).*Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          shockFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         10;\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\nwriteInterval   1;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\nmaxCo           0.2;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n    div(phi,k)        bounded Gauss upwind;\n    div(phi,epsilon)  bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)   vanLeerV;\n    reconstruct(T)   vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.001;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.001;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            symmetryPlane;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n    turbulence      on;\n    printCoeffs     on;\n\nkEpsilonCoeffs\n{\n    Cmu         0.09;\n    C1          1.44;\n    C2          1.92;\n    sigmaEps    1.3;\n    sigmaK      1.0;\n}\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder_SA": {
+    "usr_requirement": "do a offsetcylinder simulation using SpalartAllmaras turbulence model. Use PIMPLE algorithm. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-07;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell            0;\n    pRefValue           0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.5;\ndeltaT          0.0025;\n\nwriteControl    runTime;\nwriteInterval   0.05;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  8;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)       bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)   bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    right\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }    down\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    up\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    down\n    {\n        type            zeroGradient;\n    }\n    up\n    {\n        type            zeroGradient;\n    }\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n    right\n    {\n        type            zeroGradient;\n    }\n    down\n    {\n        type            noSlip;\n    }\n    up\n    {\n        type            noSlip;\n    }\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{    left\n    {\n        type            calculated;\n        value           uniform 0;\n    }    right\n    {\n        type            calculated;\n        value           uniform 0;\n    }    down\n    {\n        type            calculated;\n        value           uniform 0;\n    }    up\n    {\n        type            calculated;\n        value           uniform 0;\n    }    cylinder\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           SpalartAllmaras;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 0.01;\n\n// ************************************************************************* //\n"
+  }
+}
\ No newline at end of file
diff --git a/benchmarks/FoamBench_advanced_openfoam13_reference_qois.json b/benchmarks/FoamBench_advanced_openfoam13_reference_qois.json
new file mode 100644
index 0000000000000000000000000000000000000000..000e81cb64db589b8d21b7042c73836c5ba02233
--- /dev/null
+++ b/benchmarks/FoamBench_advanced_openfoam13_reference_qois.json
@@ -0,0 +1,11917 @@
+{
+  "cases": {
+    "Cavity_LES": {
+      "extraction": {
+        "geometry": "field-derived physics metrics plus physical-coordinate reference diagnostics",
+        "producer": "benchmarks/evaluation/basic_advanced.py",
+        "reference_run": "anonymous-reference/advanced"
+      },
+      "family": "Cavity",
+      "health": {
+        "checks": {
+          "measurement_geometry_available": true,
+          "no_proxy_fallback": true,
+          "principal_qoi_complete": true,
+          "structured_qoi_valid": true
+        },
+        "status": "pass",
+        "validation_errors": []
+      },
+      "latest_time": 10.0,
+      "metric_roles": {
+        "centerline_velocity_profiles": "principal",
+        "kinetic_energy_history": "diagnostic",
+        "response_speed_max": "principal",
+        "reverse_flow_min_u": "principal"
+      },
+      "principal_metrics": [
+        "centerline_velocity_profiles",
+        "response_speed_max",
+        "reverse_flow_min_u"
+      ],
+      "principal_qoi_group": "cavity_response",
+      "qois": {
+        "centerline_velocity_profiles": {
+          "kind": "named_profiles",
+          "profiles": [
+            {
+              "columns": [
+                "y",
+                "u",
+                "v",
+                "speed"
+              ],
+              "profile_id": "vertical_centerline",
+              "rows": [
+                [
+                  0.0025,
+                  -0.095810576,
+                  0.0038649569,
+                  0.09588849965084777
+                ],
+                [
+                  0.0075,
+                  -0.16913481,
+                  -0.0038541999999999995,
+                  0.16917871855341646
+                ],
+                [
+                  0.0125,
+                  -0.21088816,
+                  -0.0072083475,
+                  0.21101131794732328
+                ],
+                [
+                  0.0175,
+                  -0.21064913,
+                  -0.008141156,
+                  0.21080639077308172
+                ],
+                [
+                  0.0225,
+                  -0.17980266,
+                  -0.0058728362,
+                  0.1798985457087067
+                ],
+                [
+                  0.0275,
+                  -0.14258767,
+                  -0.0046560934,
+                  0.14266367036417654
+                ],
+                [
+                  0.0325,
+                  -0.1113658,
+                  -0.0047779219,
+                  0.11146824636335902
+                ],
+                [
+                  0.0375,
+                  -0.082917986,
+                  -0.0037498765000000002,
+                  0.08300273475049752
+                ],
+                [
+                  0.0425,
+                  -0.054920469,
+                  -0.0018441757,
+                  0.05495142308614429
+                ],
+                [
+                  0.0475,
+                  -0.029001855,
+                  -0.00065863415,
+                  0.029009332849698064
+                ],
+                [
+                  0.0525,
+                  -0.0048151141,
+                  0.00067104208,
+                  0.004861647999305332
+                ],
+                [
+                  0.0575,
+                  0.019540866,
+                  0.0028125312,
+                  0.01974223330276819
+                ],
+                [
+                  0.0625,
+                  0.04503617,
+                  0.0050501011,
+                  0.045318430350014566
+                ],
+                [
+                  0.0675,
+                  0.07323498,
+                  0.0073477614,
+                  0.0736026622697286
+                ],
+                [
+                  0.0725,
+                  0.10664046,
+                  0.010287184,
+                  0.1071354930154403
+                ],
+                [
+                  0.0775,
+                  0.14588685,
+                  0.01364853,
+                  0.1465239071758715
+                ],
+                [
+                  0.0825,
+                  0.18641053,
+                  0.01712606,
+                  0.1871955865558921
+                ],
+                [
+                  0.0875,
+                  0.21896354,
+                  0.017709615,
+                  0.2196785431324139
+                ],
+                [
+                  0.0925,
+                  0.2253799,
+                  0.017696106,
+                  0.22607355327762962
+                ],
+                [
+                  0.0975,
+                  0.27174124,
+                  0.006857663,
+                  0.27182775623280114
+                ]
+              ]
+            },
+            {
+              "columns": [
+                "x",
+                "u",
+                "v",
+                "speed"
+              ],
+              "profile_id": "horizontal_centerline",
+              "rows": [
+                [
+                  0.0025,
+                  0.0065253311,
+                  0.11697082,
+                  0.1171526895868679
+                ],
+                [
+                  0.0075,
+                  0.0028872883,
+                  0.17787739,
+                  0.17790082154655557
+                ],
+                [
+                  0.0125,
+                  0.0012151113,
+                  0.20747006,
+                  0.2074736183033279
+                ],
+                [
+                  0.0175,
+                  0.00027997427,
+                  0.20582758,
+                  0.20582777041557893
+                ],
+                [
+                  0.0225,
+                  0.00016974369,
+                  0.17932097,
+                  0.1793210503389415
+                ],
+                [
+                  0.0275,
+                  -7.9315616e-06,
+                  0.14253713,
+                  0.1425371302206782
+                ],
+                [
+                  0.0325,
+                  -0.00051952244,
+                  0.10739916,
+                  0.10740041653676796
+                ],
+                [
+                  0.0375,
+                  -0.0014652202,
+                  0.077499982,
+                  0.07751383154144047
+                ],
+                [
+                  0.0425,
+                  -0.0023032953,
+                  0.050681244,
+                  0.050733555588254785
+                ],
+                [
+                  0.0475,
+                  -0.003193197,
+                  0.025147162,
+                  0.025349088025707216
+                ],
+                [
+                  0.0525,
+                  -0.0048151141,
+                  0.00067104208,
+                  0.004861647999305332
+                ],
+                [
+                  0.0575,
+                  -0.0069451943,
+                  -0.023507534,
+                  0.02451203538317266
+                ],
+                [
+                  0.0625,
+                  -0.0099440511,
+                  -0.049205045,
+                  0.05019980682962273
+                ],
+                [
+                  0.0675,
+                  -0.013364754,
+                  -0.078183784,
+                  0.07931784622667948
+                ],
+                [
+                  0.0725,
+                  -0.018248075,
+                  -0.11170438,
+                  0.11318507301049033
+                ],
+                [
+                  0.0775,
+                  -0.018944424,
+                  -0.14804109,
+                  0.14924830159529412
+                ],
+                [
+                  0.0825,
+                  -0.02611714,
+                  -0.18035,
+                  0.1822312473254233
+                ],
+                [
+                  0.0875,
+                  -0.017434235,
+                  -0.20545429,
+                  0.206192671619142
+                ],
+                [
+                  0.0925,
+                  -0.041276362,
+                  -0.24904009,
+                  0.25243752590921015
+                ],
+                [
+                  0.0975,
+                  -0.02136355,
+                  -0.24649142999999998,
+                  0.24741549331447976
+                ]
+              ]
+            }
+          ]
+        },
+        "kinetic_energy_history": {
+          "kind": "time_history",
+          "points": [
+            {
+              "time": 0.0,
+              "value": 0.0
+            },
+            {
+              "time": 0.5,
+              "value": 0.001471976007375839
+            },
+            {
+              "time": 1.0,
+              "value": 0.0022233012220422978
+            },
+            {
+              "time": 1.5,
+              "value": 0.002903712194393983
+            },
+            {
+              "time": 2.0,
+              "value": 0.003570388798727527
+            },
+            {
+              "time": 2.5,
+              "value": 0.004240870490483424
+            },
+            {
+              "time": 3.0,
+              "value": 0.004925473907907507
+            },
+            {
+              "time": 3.5,
+              "value": 0.00564301348186871
+            },
+            {
+              "time": 4.0,
+              "value": 0.006378092989125182
+            },
+            {
+              "time": 4.5,
+              "value": 0.007136168753644502
+            },
+            {
+              "time": 5.0,
+              "value": 0.007888543684396761
+            },
+            {
+              "time": 5.5,
+              "value": 0.008583339964349049
+            },
+            {
+              "time": 6.0,
+              "value": 0.009216562121321851
+            },
+            {
+              "time": 6.5,
+              "value": 0.009797561956143556
+            },
+            {
+              "time": 7.0,
+              "value": 0.01031047187297122
+            },
+            {
+              "time": 7.5,
+              "value": 0.010768653999451728
+            },
+            {
+              "time": 8.0,
+              "value": 0.011182478598208272
+            },
+            {
+              "time": 8.5,
+              "value": 0.0115536350386749
+            },
+            {
+              "time": 9.0,
+              "value": 0.011890140074640001
+            },
+            {
+              "time": 9.5,
+              "value": 0.01219455491284916
+            },
+            {
+              "time": 10.0,
+              "value": 0.012471233605402086
+            }
+          ]
+        },
+        "response_speed_max": 0.41774305872467066,
+        "reverse_flow_min_u": -0.21088816
+      },
+      "source_case_id": "Cavity_LES",
+      "tolerances": {
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+                ],
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+                  4.765272269908745,
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+                ],
+                [
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+                  3.4675180014406344,
+                  4.451042,
+                  4.608020516213946
+                ]
+              ]
+            },
+            {
+              "columns": [
+                "x",
+                "p",
+                "Mach",
+                "u",
+                "speed"
+              ],
+              "profile_id": "streamline_0.75",
+              "rows": [
+                [
+                  -0.14670425,
+                  1.0,
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+                  5.0,
+                  5.0
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+                ],
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+                  4.9975803218744685,
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+                ],
+                [
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+                  1.014542621115607,
+                  4.973529541404627,
+                  4.994087462591783,
+                  4.99410425500186
+                ],
+                [
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+                  1.0261212054181053,
+                  4.953268537269935,
+                  4.989669840710676,
+                  4.989721451686543
+                ],
+                [
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+                  1.04321406476017,
+                  4.92413365204291,
+                  4.983347823891908,
+                  4.983481608128626
+                ],
+                [
+                  0.1961857774201202,
+                  1.0899533590632877,
+                  4.8488292385538765,
+                  4.966911822738667,
+                  4.967457938166147
+                ],
+                [
+                  0.20799488072196712,
+                  1.1679818849212549,
+                  4.7372357423635165,
+                  4.941710539009757,
+                  4.94351432899892
+                ],
+                [
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+                  1.340739795261321,
+                  4.527265917522146,
+                  4.89109289493058,
+                  4.897165773408599
+                ],
+                [
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+                  1.644195542002153,
+                  4.270384740292628,
+                  4.818253779920872,
+                  4.835964061001435
+                ],
+                [
+                  0.2419016903750264,
+                  2.1812597709803327,
+                  3.966772584503111,
+                  4.714676844069535,
+                  4.75741965306661
+                ],
+                [
+                  0.2529859277470944,
+                  3.0413556947529288,
+                  3.7222319458801327,
+                  4.601790272832926,
+                  4.6864582532419465
+                ],
+                [
+                  0.26510735031467564,
+                  3.9798485379264377,
+                  3.5699895373180426,
+                  4.512486124505214,
+                  4.638879359651249
+                ],
+                [
+                  0.2761847761761586,
+                  4.471234599811958,
+                  3.519234735112285,
+                  4.476490239999571,
+                  4.622138862260159
+                ],
+                [
+                  0.287616271431568,
+                  4.6850132436404435,
+                  3.4992487861397907,
+                  4.461992150354797,
+                  4.615419832103889
+                ],
+                [
+                  0.29933659932109724,
+                  4.747016516664012,
+                  3.4916084946038257,
+                  4.457445374819832,
+                  4.612976467194492
+                ]
+              ]
+            }
+          ]
+        },
+        "shock_feature_locations": {
+          "events": [
+            {
+              "coordinate": 0.09114463987854271,
+              "field": "p",
+              "local_cell_size": 0.010884357016428856,
+              "profile_id": "streamline_0.25"
+            },
+            {
+              "coordinate": 0.17142109239309317,
+              "field": "p",
+              "local_cell_size": 0.011432210587489944,
+              "profile_id": "streamline_0.50"
+            },
+            {
+              "coordinate": 0.2474438090610604,
+              "field": "p",
+              "local_cell_size": 0.011084237372067984,
+              "profile_id": "streamline_0.75"
+            }
+          ],
+          "kind": "profile_feature_locations"
+        },
+        "shock_pressure_jump_ratio": 1.3943115511574486,
+        "supersonic_volume_fraction": 1.0
+      },
+      "source_case_id": "wedge_SA",
+      "tolerances": {
+        "pressure_mach_profiles": {
+          "criterion_role": "principal_response_shape",
+          "kind": "named_profiles",
+          "normalization_floors": {
+            "Mach": 0.0001,
+            "p": 1.0,
+            "speed": 1e-05,
+            "u": 1e-05
+          },
+          "normalized_l1_max": 0.05,
+          "normalized_linf_max": 0.15,
+          "provisional": true,
+          "reference_independent": false,
+          "threshold_source": "reference_anchored_spatial_response_shape"
+        },
+        "shock_feature_locations": {
+          "kind": "profile_feature_locations",
+          "maximum_cell_offset": 2.0,
+          "physical_floor": 1e-10,
+          "provisional": true
+        },
+        "shock_pressure_jump_ratio": {
+          "criterion_role": "principal_physics",
+          "high": 2.2,
+          "kind": "physics_range",
+          "low": 1.1,
+          "provisional": true,
+          "reference_independent": true,
+          "threshold_source": "bounded_compressive_pressure_feature"
+        },
+        "supersonic_volume_fraction": {
+          "criterion_role": "principal_physics",
+          "high": 1.0,
+          "kind": "physics_range",
+          "low": 0.85,
+          "provisional": true,
+          "reference_independent": true,
+          "threshold_source": "supersonic_regime_coverage_tightened"
+        }
+      },
+      "track": "advanced"
+    }
+  },
+  "design": "foambench.basic_advanced.qoi_design",
+  "notes": [
+    "Principal scalar QoIs are reference-independent family physics criteria extracted from retained fields.",
+    "One existing spatial response profile per family is also principal and must jointly pass its reference-anchored shape tolerance.",
+    "Other histories, profiles, and feature locations remain diagnostic and do not decide Physics-grounded pass.",
+    "Provisional physical-signature and response-shape limits require future valid-alternative calibration."
+  ],
+  "openfoam_version": "Foundation v13",
+  "producer": "benchmarks/evaluation/basic_advanced.py",
+  "schema_version": "foambench.reference_qois.v2",
+  "summary": {
+    "case_count": 16,
+    "health_fail_count": 0,
+    "health_pass_count": 16,
+    "tracks": [
+      "advanced"
+    ]
+  },
+  "tolerance_policy": "physics_grounded_scalar_and_response_shape_joint_gate.v2"
+}
diff --git a/benchmarks/FoamBench_basic_openfoam13_fixed_final.json b/benchmarks/FoamBench_basic_openfoam13_fixed_final.json
new file mode 100644
index 0000000000000000000000000000000000000000..85e21d5afd74b0af8ec9057e3359dc24e2e1f838
--- /dev/null
+++ b/benchmarks/FoamBench_basic_openfoam13_fixed_final.json
@@ -0,0 +1,1922 @@
+{
+  "obliqueShock/7": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (3.5,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (3.5 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (4.0 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/6": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (3.0,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (3.0 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/3": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 3.5 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (3.5 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/5": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 3.5 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (3.5 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/2": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (3.0,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (3.0 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/4": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperaure of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/1": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (2.61933 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.9 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 1.25853;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/9": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (3.5,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (3.5 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (4.0 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/10": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (4.0,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (4.0 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (4.0 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "obliqueShock/8": {
+    "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.9 0 0);\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform (3.5 -0.50632 0);\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (4.0 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    top\n    {\n        type            fixedValue;\n        value           uniform 2.0;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.0025;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (4.1 0 0)\n    (4.1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (4.1 0 0.1)\n    (4.1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (60 30 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    top\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/7": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1100. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 5.0e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          5e-05;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1100;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.5;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/6": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1100. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          2.5e-05;\n        Pr          1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1100;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/3": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          1.82e-05;\n        Pr          1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/5": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          2.5e-05;\n        Pr          1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/2": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1500. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1500;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/4": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          2.5e-05;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/1": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/9": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 1e-4. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          1e-04;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.5;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/10": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 1e-4. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          1e-04;\n        Pr          1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.5;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "squareBend/8": {
+    "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 5.0e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        Hf          0;\n    }\n    transport\n    {\n        mu          5e-05;\n        Pr          0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 110000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n        // type            mixed;\n        refValue        uniform 110000;\n        refGradient     uniform 0;\n        valueFraction   uniform 0.3;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 110000;\n\n        // type            mixed;\n        // refValue        uniform 110000;\n        // refGradient     uniform 0;\n        // valueFraction   uniform 1;\n        // type            transonicOutletPressure;\n        // U               U;\n        // phi             phi;\n        // gamma           1.4;\n        // psi             psi;\n        // pInf            uniform 110000;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 200;\n\nboundaryField\n{\n    walls\n    {\n        type            epsilonWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 200;\n    }\n    inlet\n    {\n        type            turbulentMixingLengthDissipationRateInlet;\n        mixingLength    0.005;\n        value           uniform 200;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 200;\n        value           uniform 200;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1;\n    }\n    inlet\n    {\n        type            turbulentIntensityKineticEnergyInlet;\n        intensity       0.05;\n        value           uniform 1;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    walls\n    {\n        type            noSlip;\n    }\n\n    inlet\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    constant 0.5;\n        rhoInlet        0.5;    // Guess for rho\n        profile         turbulentBL;\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            nutkWallFunction;\n        Cmu             0.09;\n        kappa           0.41;\n        E               9.8;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1000;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        // type            zeroGradient;\n        value           uniform 1000;\n        inletValue      uniform 1000;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    walls\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-08;\n        relTol          0.1;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n\n    transonic       yes;\n    consistent      yes;\n\n    residualControl\n    {\n        p               1e-3;\n        U               1e-4;\n        h               1e-3;\n        \"(k|epsilon)\"   1e-3;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               1;\n    }\n\n    equations\n    {\n        p               1;\n        U               0.9;\n        h               0.9;\n        k               0.9;\n        epsilon         0.9;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoSimpleFoam;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.5;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\ngraphFormat     raw;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 8;\n\nmethod          hierarchical;\n\nsimpleCoeffs\n{\n    n               (8 1 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,h)          bounded Gauss upwind;\n\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n\n    div(phi,K)          bounded Gauss upwind;\n\n    div(phid,p)         Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.001;\n\nvertices\n(\n    // front-plane: z = +25mm\n    // inlet region\n    (   -50  25   25)           // pt 0\n    (     0  25   25)           // pt 1\n    (   -50  75   25)           // pt 2\n    (     0  75   25)           // pt 3\n    // outlet region\n    (  -500 -75   25)           // pt 4\n    (     0 -75   25)           // pt 5\n    (  -500 -25   25)           // pt 6\n    (     0 -25   25)           // pt 7\n    // bend mid-points\n    (    25   0   25)           // pt 8\n    (    75   0   25)           // pt 9\n    // back-plane: z = -25mm\n    // inlet region\n    (   -50  25   -25)          // pt 0 + 10\n    (     0  25   -25)          // pt 1 + 10\n    (   -50  75   -25)          // pt 2 + 10\n    (     0  75   -25)          // pt 3 + 10\n    // outlet region\n    (  -500 -75   -25)          // pt 4 + 10\n    (     0 -75   -25)          // pt 5 + 10\n    (  -500 -25   -25)          // pt 7 + 10\n    (     0 -25   -25)          // pt 8 + 10\n    // bend mid-points\n    (    25   0   -25)          // pt 8 + 10\n    (    75   0   -25)          // pt 9 + 10\n);\n\nblocks\n(\n    hex (0 1 11 10  2 3 13 12) inlet  ( 20 20 20)  simpleGrading (1 1 1)\n    hex (4 5 15 14  6 7 17 16) outlet (200 20 20)  simpleGrading (1 1 1)\n\n    hex (1 8 18 11  3 9 19 13) bend1  ( 30 20 20)  simpleGrading (1 1 1)\n    hex (5 9 19 15  7 8 18 17) bend2  ( 30 20 20)  simpleGrading (1 1 1)\n);\n\nedges\n(\n   // block 2\n   arc  1  8  ( 17.678  17.678  25)\n   arc 11 18  ( 17.678  17.678 -25)\n   arc  3  9  ( 53.033  53.033  25)\n   arc 13 19  ( 53.033  53.033 -25)\n   // block 3\n   arc  7  8  ( 17.678  -17.678  25)\n   arc 17 18  ( 17.678  -17.678 -25)\n   arc  5  9  ( 53.033  -53.033  25)\n   arc 15 19  ( 53.033  -53.033 -25)\n);\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 2 12 10)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 6 16 14)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n(0 1 3 2)\n            (10 12 13 11)\n            (0 10 11 1)\n            (2 3 13 12)\n            (4 5 7 6)\n            (14 16 17 15)\n            (4 14 15 5)\n            (6 7 17 16)\n            (1 8 9 3)\n            (11 13 19 18)\n            (1 11 18 8)\n            (3 9 19 13)\n            (5 9 8 7)\n            (15 17 18 19)\n            (5 15 19 9)\n            (7 8 18 17)\n        );\n    }\n\n);\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    minFactor  0.1;\n    maxFactor  2;\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/7": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/6": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/3": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/5": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/2": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/4": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/1": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-5 and viscosity of water to be 1e-6. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-06;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1.48e-05;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/9": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1.48e-05;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/10": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1.48e-05;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "damBreakWithObstacle/8": {
+    "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 -9.81);\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water air);\n\nsigma           0.07;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1.48e-05;\n\nrho             1;\n\n\n// ************************************************************************* //\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    // How often to refine\n    refineInterval  1;\n\n    // Field to be refinement on\n    field           alpha.water;\n\n    // Refine field in between lower..upper\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    // Have slower than 2:1 refinement\n    nBufferLayers   1;\n\n    // Refine cells only up to maxRefinement levels\n    maxRefinement   2;\n\n    // Stop refinement if maxCells reached\n    maxCells        200000;\n\n    // Flux field and corresponding velocity field. Fluxes on changed\n    // faces get recalculated by interpolating the velocity. Use 'none'\n    // on surfaceScalarFields that do not need to be reinterpolated.\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (ghf none)\n    );\n\n    // Write the refinement level as a volScalarField\n    dumpLevel       true;\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            prghTotalPressure;\n        rho             rho;\n        psi             none;\n        gamma           1;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            fixedFluxPressure;\n        gradient        uniform 0;\n        value           uniform 0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    constant (0 0 0);\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00015;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.00015;\n        value           uniform 0.00015;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00015;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      binary;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    atmosphere\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    walls\n    {\n        type            uniformFixedValue;\n        uniformValue    \n        {\n            type            constant;\n            value           (0 0 0);\n        }\n        value           uniform (0 0 0);\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 5e-07;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            nutkRoughWallFunction;\n        Ks              uniform 0.0001;\n        Cs              uniform 0.5;\n        value           uniform 5e-07;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 2;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 2;\n        value           uniform 2;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 2;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    atmosphere\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 3;\n        nLimiterIter    5;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        tolerance       1e-08;\n        relTol          0.01;\n        smoother        DIC;\n        cacheAgglomeration no;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p_rghFinal;\n        tolerance       1e-4;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n        nSweeps         1;\n    }\n\n    \"(k|omega|B|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefPoint      (0.51 0.51 0.51);\n    pRefValue      0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     interFoam;\nsolver          incompressibleVoF;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          0.001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      topoSetDict;\n}\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    c0;\n        type    cellSet;\n        action  clear;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  invert;\n    }\n    {\n        name    c0;\n        type    cellSet;\n        action  delete;\n        source  boxToCell;\n        box     (0.375 0.375 0) (0.625 0.625 0.25);\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  6;\n\nmethod              scotch;\n\nsimpleCoeffs\n{\n    n               (2 2 1);\n}\n\nhierarchicalCoeffs\n{\n    n               (2 2 1);\n    order           xyz;\n}\n\nmanualCoeffs\n{\n    dataFile        \"\";\n}\n\ndistributed     no;\n\nroots           ( );\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)   Gauss upwind;\n    div(phi,alpha)  Gauss MPLIC;\n    div(phi,k)      Gauss upwind;\n    div(phi,omega)  Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 1)\n    (1 0 1)\n    (1 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    atmosphere\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    alpha.water     0;\n    U               (0 0 0);\n}\n\nzones\n{\n    waterColumn\n    {\n        type        box;\n        zoneType    cell;\n\n        box         (0 0 0) (0.6 0.1875 0.75);\n\n        values\n        {\n            alpha.water 1;\n        }\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/7": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/6": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/3": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/5": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/2": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/4": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/1": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 10m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-5. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1e-05;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (10 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/9": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (25 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/10": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (25 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "pitzDaily/8": {
+    "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    upperWall\n    {\n        type            zeroGradient;\n    }\n\n    lowerWall\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 14.855;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 14.855;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    lowerWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 14.855;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.375;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 0.375;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    upperWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    lowerWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (25 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    upperWall\n    {\n        type            noSlip;\n    }\n\n    lowerWall\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    upperWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    lowerWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver           GAMG;\n        tolerance        1e-7;\n        relTol           0.01;\n\n        smoother         DICGaussSeidel;\n\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.3;\n\ndeltaT          0.0001;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           5;\n\nfunctions\n{\n    #includeFunc patchAverage(patch=inlet, fields=(p U))\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,k)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,R)          Gauss upwind;\n    div(R)              Gauss linear;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Note: this file is a Copy of $FOAM_TUTORIALS/resources/blockMesh/pitzDaily\n\nconvertToMeters 0.001;\n\nvertices\n(\n    (-20.6 0 -0.5)\n    (-20.6 25.4 -0.5)\n    (0 -25.4 -0.5)\n    (0 0 -0.5)\n    (0 25.4 -0.5)\n    (206 -25.4 -0.5)\n    (206 0 -0.5)\n    (206 25.4 -0.5)\n    (290 -16.6 -0.5)\n    (290 0 -0.5)\n    (290 16.6 -0.5)\n\n    (-20.6 0 0.5)\n    (-20.6 25.4 0.5)\n    (0 -25.4 0.5)\n    (0 0 0.5)\n    (0 25.4 0.5)\n    (206 -25.4 0.5)\n    (206 0 0.5)\n    (206 25.4 0.5)\n    (290 -16.6 0.5)\n    (290 0 0.5)\n    (290 16.6 0.5)\n);\n\nnegY\n(\n    (2 4 1)\n    (1 3 0.3)\n);\n\nposY\n(\n    (1 4 2)\n    (2 3 4)\n    (2 4 0.25)\n);\n\nposYR\n(\n    (2 1 1)\n    (1 1 0.25)\n);\n\n\nblocks\n(\n    hex (0 3 4 1 11 14 15 12)\n    (18 30 1)\n    simpleGrading (0.5 $posY 1)\n\n    hex (2 5 6 3 13 16 17 14)\n    (180 27 1)\n    edgeGrading (4 4 4 4 $negY 1 1 $negY 1 1 1 1)\n\n    hex (3 6 7 4 14 17 18 15)\n    (180 30 1)\n    edgeGrading (4 4 4 4 $posY $posYR $posYR $posY 1 1 1 1)\n\n    hex (5 8 9 6 16 19 20 17)\n    (25 27 1)\n    simpleGrading (2.5 1 1)\n\n    hex (6 9 10 7 17 20 21 18)\n    (25 30 1)\n    simpleGrading (2.5 $posYR 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 12 11)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (8 9 20 19)\n            (9 10 21 20)\n        );\n    }\n    upperWall\n    {\n        type wall;\n        faces\n        (\n            (1 4 15 12)\n            (4 7 18 15)\n            (7 10 21 18)\n        );\n    }\n    lowerWall\n    {\n        type wall;\n        faces\n        (\n            (0 3 14 11)\n            (3 2 13 14)\n            (2 5 16 13)\n            (5 8 19 16)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 4 1)\n            (2 5 6 3)\n            (3 6 7 4)\n            (5 8 9 6)\n            (6 9 10 7)\n            (11 14 15 12)\n            (13 16 17 14)\n            (14 17 18 15)\n            (16 19 20 17)\n            (17 20 21 18)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/7": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.4 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/6": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.3 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.3 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.3 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/3": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.1 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.2 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/5": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.3 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.2 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/2": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.2 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.2 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/4": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.3 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/1": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.1 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/9": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.3 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.1 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.1 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/10": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.4 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.4 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.4 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "counterFlowFlame2D/8": {
+    "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"multicomponentFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/combustionProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      combustionProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ncombustionModel  laminar;\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/chemistryProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      chemistryProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nchemistryType\n{\n    solver            EulerImplicit;\n}\n\nchemistry           on;\n\ninitialChemicalTimeStep 1e-07;\n\nEulerImplicitCoeffs\n{\n    cTauChem        1;\n}\n\nodeCoeffs\n{\n    solver          Rosenbrock43;\n    absTol          1e-8;\n    relTol          0.01;\n}\n\n#include \"reactions\"\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         coefficientWilkeMulticomponentMixture;\n    transport       sutherland;\n    thermo          janaf;\n    energy          sensibleEnthalpy;\n    equationOfState perfectGas;\n    specie          specie;\n}\n\ndefaultSpecie N2;\n\n#include \"thermo.compressibleGas\"\n\n// ************************************************************************* //\n",
+    "constant/thermo.compressibleGas": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\n\nspecies\n(\n    O2\n    H2O\n    CH4\n    CO2\n    N2\n);\n\nO2\n{\n    specie\n    {\n        molWeight       31.9988;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 3.69758 0.00061352 -1.25884e-07 1.77528e-11 -1.13644e-15 -1233.93 3.18917 );\n        lowCpCoeffs     ( 3.21294 0.00112749 -5.75615e-07 1.31388e-09 -8.76855e-13 -1005.25 6.03474 );\n    }\n    transport\n    {\n        As              1.753e-6;\n        Ts              139;\n    }\n}\n\nH2O\n{\n    specie\n    {\n        molWeight       18.0153;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.67215 0.00305629 -8.73026e-07 1.201e-10 -6.39162e-15 -29899.2 6.86282 );\n        lowCpCoeffs     ( 3.38684 0.00347498 -6.3547e-06 6.96858e-09 -2.50659e-12 -30208.1 2.59023 );\n    }\n    transport\n    {\n        As              2.978e-7;\n        Ts              1064;\n    }\n}\n\nCH4\n{\n    specie\n    {\n        molWeight       16.0428;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           6000;\n        Tcommon         1000;\n        highCpCoeffs    ( 1.63543 0.0100844 -3.36924e-06 5.34973e-10 -3.15528e-14 -10005.6 9.9937 );\n        lowCpCoeffs     ( 5.14988 -0.013671 4.91801e-05 -4.84744e-08 1.66694e-11 -10246.6 -4.64132 );\n    }\n    transport\n    {\n        As              1.0194e-06;\n        Ts              171.06;\n    }\n}\n\nCO2\n{\n    specie\n    {\n        molWeight       44.01;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 4.45362 0.00314017 -1.27841e-06 2.394e-10 -1.66903e-14 -48967 -0.955396 );\n        lowCpCoeffs     ( 2.27572 0.00992207 -1.04091e-05 6.86669e-09 -2.11728e-12 -48373.1 10.1885 );\n    }\n    transport\n    {\n        As              1.503e-6;\n        Ts              222;\n    }\n}\n\nN2\n{\n    specie\n    {\n        molWeight       28.0134;\n    }\n    thermodynamics\n    {\n        Tlow            200;\n        Thigh           5000;\n        Tcommon         1000;\n        highCpCoeffs    ( 2.92664 0.00148798 -5.68476e-07 1.0097e-10 -6.75335e-15 -922.798 5.98053 );\n        lowCpCoeffs     ( 3.29868 0.00140824 -3.96322e-06 5.64152e-09 -2.44486e-12 -1020.9 3.95037 );\n    }\n    transport\n    {\n        As              1.401e-6;\n        Ts              107;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/reactions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nReference:\n    Bui-Pham, M. N. (1992).\n    Studies in structures of lam inar hydrocarbon flames.\n    PhD Thesis, University of California, San Diego\n\nNotes:\n    This mechanism was developed for simulating this exact counter-flow flame\n    configuration. It should not be considered general-purpose.\n\n\\*---------------------------------------------------------------------------*/\n\nreactions\n{\n    methaneReaction\n    {\n        type     irreversibleArrhenius;\n        reaction \"CH4 + 2O2 = CO2 + 2H2O\";\n        A        5.2e16;\n        beta     0;\n        Ta       14906;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/Ydefault": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ydefault;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/H2O": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      H2O;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1e5;\n\nboundaryField\n{\n    fuel\n    {\n        type            zeroGradient;\n    }\n    air\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            totalPressure;\n        p0              $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CH4": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CH4;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0.0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 1.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0.0;\n        value           uniform 0.0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/Qdot": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Qdot;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -3 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    air\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/CO2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      CO2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform (0.4 0 0);\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform (-0.2 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 2000;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 293;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 293;\n        value           uniform 293;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/O2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      O2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.23;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 0;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/N2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      N2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    fuel\n    {\n        type            fixedValue;\n        value           uniform 0.0;\n    }\n    air\n    {\n        type            fixedValue;\n        value           uniform 0.77;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          1e-06;\n\ndeltaT0         1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-6;\n        relTol          0.0;\n    }\n\n    \"(U|h|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|h|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n    Yi\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    YiFinal\n    {\n        $Yi;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nOuterCorrectors  1;\n    nCorrectors       2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     reactingFoam;\nsolver          multicomponentFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          1e-6;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.4;\n\nfunctions\n{\n    #includeFunc Qdot\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,Yi_h)   Gauss limitedLinear 1;\n    div(phi,K)      Gauss limitedLinear 1;\n    div(phid,p)     Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,k) Gauss limitedLinear 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc Qdot\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0  -0.01 -0.01)\n    (0.02 -0.01 -0.01)\n    (0.02  0.01 -0.01)\n    (0.0   0.01 -0.01)\n    (0.0  -0.01  0.01)\n    (0.02 -0.01  0.01)\n    (0.02  0.01  0.01)\n    (0.0   0.01  0.01)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (100 40 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    fuel\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    air\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (7 6 2 3)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (4 5 6 7)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/7": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.1m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.1 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.1 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (2.1 0 0);\n        value           uniform (2.1 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/6": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.9m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1.9 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (1.9 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (1.9 0 0);\n        value           uniform (1.9 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/3": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1.3 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (1.3 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (1.3 0 0);\n        value           uniform (1.3 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/5": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.7m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1.7 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (1.7 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (1.7 0 0);\n        value           uniform (1.7 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/2": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.1m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1.1 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (1.1 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (1.1 0 0);\n        value           uniform (1.1 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/4": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.5m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1.5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (1.5 0 0);\n        value           uniform (1.5 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/1": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (4 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (4 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (4 0 0);\n        value           uniform (4 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/9": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.5m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.5 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (2.5 0 0);\n        value           uniform (2.5 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/10": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.7m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.7 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.7 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (2.7 0 0);\n        value           uniform (2.7 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "forwardStep/8": {
+    "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n// Note: these are the properties for a \"normalised\" inviscid gas\n//       for which the speed of sound is 1 m/s at a temperature of 1K\n//       and gamma = 7/5\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (2.3 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (2.3 0 0);\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (2.3 0 0);\n        value           uniform (2.3 0 0);\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 1;\n        value           uniform 1;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n    \n    rhoFinal\n    {\n        solver          PCG;  // Preconditioned Conjugate Gradient\n        preconditioner  DIC; // Diagonal incomplete-Cholesky\n        tolerance       1e-05;\n        relTol          0;\n    }\n    \n    UFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n    eFinal\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    nCorrectors         2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         4;\n\ndeltaT          0.002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       1;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -0.05)\n    (0.6 0 -0.05)\n    (0 0.2 -0.05)\n    (0.6 0.2 -0.05)\n    (3 0.2 -0.05)\n    (0 1 -0.05)\n    (0.6 1 -0.05)\n    (3 1 -0.05)\n    (0 0 0.05)\n    (0.6 0 0.05)\n    (0 0.2 0.05)\n    (0.6 0.2 0.05)\n    (3 0.2 0.05)\n    (0 1 0.05)\n    (0.6 1 0.05)\n    (3 1 0.05)\n);\n\nblocks\n(\n    hex (0 1 3 2 8 9 11 10) (48 16 1) simpleGrading (1 1 1)\n    hex (2 3 6 5 10 11 14 13) (48 64 1) simpleGrading (1 1 1)\n    hex (3 4 7 6 11 12 15 14) (192 64 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 8 10 2)\n            (2 10 13 5)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (4 7 15 12)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 9 8)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 3 11 9)\n            (3 4 12 11)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/7": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 310;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 295;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/6": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 305;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 290;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/3": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 310;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/5": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 305;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 295;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/2": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 305;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/4": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 315;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/1": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t=1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 301 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\n        type            noSlip;\n    }\n    ceiling\n    {\n        type            noSlip;\n    }\n    sideWalls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 301;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\n        type            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\n        type            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\n        type            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/9": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 315;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 295;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/10": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 315;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 290;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "BernardCells/8": {
+    "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 -9.81 0);\n\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState Boussinesq;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       18;\n    }\n    equationOfState\n    {\n        rho0            1;\n        T0              300;\n        beta            1e-03;\n    }\n    thermodynamics\n    {\n        Cv              712;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1e-03;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            fixedFluxPressure;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            calculated;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            epsilonWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    floor\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            kqRWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1e-4 0 0);\n\nboundaryField\n{\n    floor\n    {\ntype            noSlip;\n    }\n    ceiling\n    {\ntype            noSlip;\n    }\n    sideWalls\n    {\ntype            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            nutkWallFunction;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    floor\n    {\n        type            fixedValue;\n        value           uniform 310;\n    }\n    ceiling\n    {\n        type            fixedValue;\n        value           uniform 290;\n    }\n    sideWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    floor\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    ceiling\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    sideWalls\n    {\ntype            compressible::alphatJayatillekeWallFunction;\n        Prt             0.85;\n        value           $internalField;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|e|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nNonOrthogonalCorrectors 0;\n    nCorrectors       2;\n\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"   1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     buoyantFoam;\nsolver          fluid;\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    runTime;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nfunctions\n{\n    #includeFunc residuals(p_rgh)\n    #includeFunc streamlinesLine(funcName=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind grad(U);\n    div(phi,e)          Gauss limitedLinear 1;\n\n    turbulence          Gauss limitedLinear 1;\n    div(phi,k)          $turbulence;\n    div(phi,epsilon)    $turbulence;\n\n    div(phi,(p|rho))    Gauss limitedLinear 1;\n    div(phi,K)          Gauss linear;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc residuals(p_rgh)\n#includeFunc streamlinesLine(name=streamlines, start=(0 0.5 0), end=(9 0.5 0), nPoints=24, U)\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 -1)\n    (9 0 -1)\n    (9 1 -1)\n    (0 1 -1)\n    (0 0 1)\n    (9 0 1)\n    (9 1 1)\n    (0 1 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 10 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    floor\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n\n    ceiling\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n\n    sideWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/7": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/6": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/3": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (10 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 2;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.0001;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/5": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (15 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 3;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/2": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (10 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.0001;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/4": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (10 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 3;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.0001;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/1": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 5 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (5 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.0001;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/9": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1.0;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 3;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/10": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1.5;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 3;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "wedge/8": {
+    "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    // normalised gas\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              0.71;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (5 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (20 0 0);\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 3;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    bottom\n    {\n        type            symmetryPlane;\n    }\n\n    top\n    {\n        type            symmetryPlane;\n    }\n\n    obstacle\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\n\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     rhoCentralFoam;\nsolver          shockFluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.2;\n\ndeltaT          0.00005;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           1;\n\nmaxDeltaT       1e-06;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(tauMC)      Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-0.15242 0       -0.005)\n    ( 0       0       -0.005)\n    ( 0.3048  0.081670913853  -0.005)\n    (-0.15242 0.1524 -0.005)\n    ( 0       0.1524 -0.005)\n    ( 0.3048  0.1524 -0.005)\n\n    (-0.15242 0        0.005)\n    ( 0       0        0.005)\n    ( 0.3048  0.081670913853 0.005)\n    (-0.15242 0.1524  0.005)\n    ( 0       0.1524  0.005)\n    ( 0.3048  0.1524  0.005)\n\n);\n\nblocks\n(\n    hex (0 1 4 3 6 7 10 9 ) (40 40 1) simpleGrading (1 1 1)\n    hex (1 2 5 4 7 8 11 10) (80 40 1) simpleGrading (1 1 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 6 9 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 5 11 8)\n        );\n    }\n    bottom\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 1 7 6)\n        );\n    }\n    top\n    {\n        type symmetryPlane;\n        faces\n        (\n            (3 9 10 4)\n            (4 10 11 5)\n        );\n    }\n    obstacle\n    {\n        type patch;\n        faces\n        (\n            (1 2 8 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/7": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.07 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.07;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.07;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.07;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 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0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.009\n0.009\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.009\n0.009\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n0.07\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.07\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/6": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.06 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.06;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.06;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.06;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 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0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.009\n0.009\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.009\n0.009\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n0.06\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.06\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/3": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.03 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.03;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.03;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.03;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.009\n0.009\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.009\n0.009\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n0.03\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.03\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/5": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.05 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.05;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.05;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.05;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.009\n0.009\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.009\n0.009\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n0.05\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.05\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/2": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.02 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.02;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.02;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.02;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.009\n0.009\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.009\n0.009\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n0.02\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.02\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/4": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.04 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.04;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.04;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.04;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.009\n0.009\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.009\n0.009\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n0.04\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.04\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/1": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.01 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.01;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.01;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.009\n0.009\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.009\n0.009\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n0.01\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.01\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/9": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.09 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.09;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.09;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.09;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.009\n0.009\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.009\n0.009\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n0.09\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.09\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/10": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.1 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.1;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.1;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.1;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.009\n0.009\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.009\n0.009\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n0.1\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.1\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "shallowWaterWithSquareBump/8": {
+    "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.08 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\napplication=\"shallowWaterFoam\"\n\nrunApplication blockMesh\nrunApplication $application\n\n#------------------------------------------------------------------------------\n",
+    "constant/h0": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"constant\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0.001\n0.001\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n0\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/h0.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h0;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "constant/gravitationalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      gravitationalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ng            g           [0 1 -2 0 0 0 0]  (0 0 -9.81);\nrotating     true;\nOmega        Omega       [0 0 -1 0 0 0 0]  (0 0 7.292e-5);\n\n// ************************************************************************* //\n",
+    "0/hTotal": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      hTotal;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            calculated;\n        value           uniform 0.08;\n    }\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.08;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.08;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   nonuniform List<vector> \n400\n(\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.0009 0 0)\n(0.0009 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n(0.001 0 0)\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h.orig;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/h": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      h;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 0 0 0 0 0];\n\ninternalField   nonuniform List<scalar> \n400\n(\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.009\n0.009\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.009\n0.009\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n0.08\n)\n;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0.01;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/hU.orig": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      hU;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform (0.001 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            slip;\n    }\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (0.001 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    h\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0.01;\n    }\n\n    hFinal\n    {\n        $h;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    hU\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    hUFinal\n    {\n        $hU;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 3;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n\n    momentumPredictor yes;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     shallowWaterFoam;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          0.1;\n\nwriteControl    runTime;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable false;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         CrankNicolson 0.9;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phiv,hU)    Gauss LUST un;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear uncorrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         uncorrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n            (1 5 4 0)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 4 7 3)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (2 6 5 1)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue h0 0\n    volScalarFieldValue h 0.08\n    volVectorFieldValue hU (0.001 0 0)\n);\n\nregions\n(\n    boxToCell\n    {\n        box (0.45 0.45 0) (0.55 0.55 0.1);\n\n        fieldValues\n        (\n            volScalarFieldValue h0 0.001\n            volScalarFieldValue h  0.009\n            volVectorFieldValue hU  (0.0009 0 0)\n        );\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/7": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/6": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/3": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulations runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/5": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/2": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/4": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/1": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/9": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-04 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/10": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cavity/8": {
+    "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-05 [m^2/s];\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            zeroGradient;\n    }\n\n    fixedWalls\n    {\n        type            zeroGradient;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.00754;\n\nboundaryField\n{\n    movingWall\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    fixedWalls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.00754;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.00375;\n\nboundaryField\n{\n    movingWall\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    fixedWalls\n    {\n        type            kqRWallFunction;\n        value           uniform 0.00375;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    movingWall\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    fixedWalls\n    {\n        type            noSlip;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    movingWall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    fixedWalls\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 22.4;\n\nboundaryField\n{\n    movingWall\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    fixedWalls\n    {\n        type            omegaWallFunction;\n        value           uniform 22.4;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        tolerance       1e-06;\n        relTol          0.1;\n        smoother        GaussSeidel;\n    }\n\n    pFinal\n    {\n        $p;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|R|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-05;\n        relTol          0;\n    }\n}\n\nPISO\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n\nPIMPLE\n{\n    nCorrectors     2;\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pisoFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10.0;\n\ndeltaT          0.005;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      Gauss limitedLinearV 1;\n    div(phi,k)      Gauss limitedLinear 1;\n    div(phi,epsilon) Gauss limitedLinear 1;\n    div(phi,omega)  Gauss limitedLinear 1;\n    div(phi,R)      Gauss limitedLinear 1;\n    div(R)          Gauss linear;\n    div(phi,nuTilda) Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 1 0)\n    (0 1 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 1 0.1)\n    (0 1 0.1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    movingWall\n    {\n        type wall;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    fixedWalls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n            (1 5 4 0)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 3 2 1)\n            (4 5 6 7)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/7": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-01;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/6": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-02;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/3": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-02;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/5": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (2 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/2": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/4": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-01;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1.5 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/1": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.01;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (1 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/9": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-02;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/10": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-01;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  },
+  "Cylinder/8": {
+    "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model        generalisedNewtonian;\n\n    viscosityModel CrossPowerLaw;\n\n    nuInf           10;\n    m               0.4;\n    n               3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-03;\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            zeroGradient;\n    }\n\n    right\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    down\n    {\n        type            zeroGradient;\n    }\n\n    up\n    {\n        type            zeroGradient;\n    }\n\n    cylinder\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            fixedValue;\n        value           uniform (3 0 0);\n    }\n\n    right\n    {\n        type            zeroGradient;\n    }\n\n    down\n    {\n        type            noSlip;\n    }\n\n    up\n    {\n        type            noSlip;\n    }\n\n    cylinder\n    {\n        type            noSlip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"U.*\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n\n        tolerance       1e-5;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   no;\n    nOuterCorrectors    5;\n    nCorrectors         1;\n    nNonOrthogonalCorrectors 0;\n    transportPredictionFirst yes;\n}\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     pimpleFoam;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.5;\n\ndeltaT          0.0025;\n\nwriteControl    runTime;\n\nwriteInterval   0.05;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         leastSquares;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      Gauss linear;\n    div((nuEff*dev2(T(grad(U)))))  Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (1 0 -1)\n    (1.4 0 -1)\n    (5 0 -1)\n    (5 0.989949 -1)\n    (0.989949 0.989949 -1)\n    (0.707107 0.707107 -1)\n    (5 2.5 -1)\n    (0.989949 2.5 -1)\n    (0 2.5 -1)\n    (0 1.4 -1)\n    (0 1 -1)\n    (-1 0 -1)\n    (-1.4 0 -1)\n    (-5 0 -1)\n    (-5 0.989949 -1)\n    (-0.989949 0.989949 -1)\n    (-0.707107 0.707107 -1)\n    (-5 2.5 -1)\n    (-0.989949 2.5 -1)\n    (5 -0.989949 -1)\n    (0.989949 -0.989949 -1)\n    (0.707107 -0.707107 -1)\n    (5 -1.5 -1)\n    (0.989949 -1.5 -1)\n    (0 -1.5 -1)\n    (0 -1.4 -1)\n    (0 -1 -1)\n    (-5 -0.989949 -1)\n    (-0.989949 -0.989949 -1)\n    (-0.707107 -0.707107 -1)\n    (-5 -1.5 -1)\n    (-0.989949 -1.5 -1)\n    (1 0 1)\n    (1.4 0 1)\n    (5 0 1)\n    (5 0.989949 1)\n    (0.989949 0.989949 1)\n    (0.707107 0.707107 1)\n    (5 2.5 1)\n    (0.989949 2.5 1)\n    (0 2.5 1)\n    (0 1.4 1)\n    (0 1 1)\n    (-1 0 1)\n    (-1.4 0 1)\n    (-5 0 1)\n    (-5 0.989949 1)\n    (-0.989949 0.989949 1)\n    (-0.707107 0.707107 1)\n    (-5 2.5 1)\n    (-0.989949 2.5 1)\n    (5 -0.989949 1)\n    (0.989949 -0.989949 1)\n    (0.707107 -0.707107 1)\n    (5 -1.5 1)\n    (0.989949 -1.5 1)\n    (0 -1.5 1)\n    (0 -1.4 1)\n    (0 -1 1)\n    (-5 -0.989949 1)\n    (-0.989949 -0.989949 1)\n    (-0.707107 -0.707107 1)\n    (-5 -1.5 1)\n    (-0.989949 -1.5 1)\n);\n\nblocks\n(\n    hex (5 4 9 10 37 36 41 42) (10 10 1) simpleGrading (1 1 1)\n    hex (0 1 4 5 32 33 36 37) (10 10 1) simpleGrading (1 1 1)\n    hex (1 2 3 4 33 34 35 36) (10 10 1) simpleGrading (1 1 1)\n    hex (4 3 6 7 36 35 38 39) (10 10 1) simpleGrading (1 1 1)\n    hex (9 4 7 8 41 36 39 40) (10 10 1) simpleGrading (1 1 1)\n    hex (15 16 10 9 47 48 42 41) (10 10 1) simpleGrading (1 1 1)\n    hex (12 11 16 15 44 43 48 47) (10 10 1) simpleGrading (1 1 1)\n    hex (13 12 15 14 45 44 47 46) (10 10 1) simpleGrading (1 1 1)\n    hex (14 15 18 17 46 47 50 49) (10 10 1) simpleGrading (1 1 1)\n    hex (15 9 8 18 47 41 40 50) (10 10 1) simpleGrading (1 1 1)\n    hex (26 25 20 21 58 57 52 53) (10 10 1) simpleGrading (1 1 1)\n    hex (21 20 1 0 53 52 33 32) (10 10 1) simpleGrading (1 1 1)\n    hex (20 19 2 1 52 51 34 33) (10 10 1) simpleGrading (1 1 1)\n    hex (23 22 19 20 55 54 51 52) (10 5 1) simpleGrading (1 1 1)\n    hex (24 23 20 25 56 55 52 57) (10 5 1) simpleGrading (1 1 1)\n    hex (28 29 11 12 60 61 43 44) (10 10 1) simpleGrading (1 1 1)\n    hex (25 26 29 28 57 58 61 60) (10 10 1) simpleGrading (1 1 1)\n    hex (27 28 12 13 59 60 44 45) (10 10 1) simpleGrading (1 1 1)\n    hex (30 31 28 27 62 63 60 59) (10 5 1) simpleGrading (1 1 1)\n    hex (31 24 25 28 63 56 57 60) (10 5 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n    arc 5 0 (0.92388 0.382683 -1)\n    arc 5 10 (0.382683 0.923879 -1)\n    arc 1 4 (1.29343 0.535757 -1)\n    arc 4 9 (0.535757 1.29343 -1)\n    arc 32 37 (0.92388 0.382683 1)\n    arc 37 42 (0.382683 0.923879 1)\n    arc 33 36 (1.29343 0.535757 1)\n    arc 36 41 (0.535757 1.29343 1)\n    arc 11 16 (-0.923879 0.382683 -1)\n    arc 16 10 (-0.382683 0.923879 -1)\n    arc 12 15 (-1.29343 0.535757 -1)\n    arc 15 9 (-0.535757 1.29343 -1)\n    arc 43 48 (-0.923879 0.382683 1)\n    arc 48 42 (-0.382683 0.923879 1)\n    arc 44 47 (-1.29343 0.535757 1)\n    arc 47 41 (-0.535757 1.29343 1)\n    arc 0 21 (0.923879 -0.382683 -1)\n    arc 21 26 (0.382683 -0.923879 -1)\n    arc 1 20 (1.29343 -0.535757 -1)\n    arc 20 25 (0.535757 -1.29343 -1)\n    arc 32 53 (0.923879 -0.382683 1)\n    arc 53 58 (0.382683 -0.923879 1)\n    arc 33 52 (1.29343 -0.535757 1)\n    arc 52 57 (0.535757 -1.29343 1)\n    arc 11 29 (-0.923879 -0.382683 -1)\n    arc 29 26 (-0.382683 -0.923879 -1)\n    arc 12 28 (-1.29343 -0.535757 -1)\n    arc 28 25 (-0.535757 -1.29343 -1)\n    arc 43 61 (-0.923879 -0.382683 1)\n    arc 61 58 (-0.382683 -0.923879 1)\n    arc 44 60 (-1.29343 -0.535757 1)\n    arc 60 57 (-0.535757 -1.29343 1)\n);\n\ndefaultPatch\n{\n    type empty;\n}\n\nboundary\n(\n    left\n    {\n        type patch;\n        faces\n        (\n            (17 14 46 49)\n            (14 13 45 46)\n            (13 27 59 45)\n            (27 30 62 59)\n        );\n    }\n    right\n    {\n        type patch;\n        faces\n        (\n            (22 19 51 54)\n            (19 2 34 51)\n            (2 3 35 34)\n            (3 6 38 35)\n        );\n    }\n    down\n    {\n        type wall;\n        faces\n        (\n            (30 31 63 62)\n            (31 24 56 63)\n            (24 23 55 56)\n            (23 22 54 55)\n        );\n    }\n    up\n    {\n        type wall;\n        faces\n        (\n            (6 7 39 38)\n            (7 8 40 39)\n            (8 18 50 40)\n            (18 17 49 50)\n        );\n    }\n    cylinder\n    {\n        type wall;\n        faces\n        (\n            (0 5 37 32)\n            (5 10 42 37)\n            (10 16 48 42)\n            (16 11 43 48)\n            (11 29 61 43)\n            (29 26 58 61)\n            (26 21 53 58)\n            (21 0 32 53)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n"
+  }
+}
\ No newline at end of file
diff --git a/benchmarks/FoamBench_basic_openfoam13_reference_qois.json b/benchmarks/FoamBench_basic_openfoam13_reference_qois.json
new file mode 100644
index 0000000000000000000000000000000000000000..e0d885d290d0ae618d920dea2e738ab3d0b4bb49
--- /dev/null
+++ b/benchmarks/FoamBench_basic_openfoam13_reference_qois.json
@@ -0,0 +1,69703 @@
+{
+  "cases": {
+    "BernardCells/1": {
+      "extraction": {
+        "geometry": "field-derived physics metrics plus physical-coordinate reference diagnostics",
+        "producer": "benchmarks/evaluation/basic_advanced.py",
+        "reference_run": "anonymous-reference/basic"
+      },
+      "family": "BernardCells",
+      "health": {
+        "checks": {
+          "measurement_geometry_available": true,
+          "no_proxy_fallback": true,
+          "principal_qoi_complete": true,
+          "structured_qoi_valid": true
+        },
+        "status": "pass",
+        "validation_errors": []
+      },
+      "latest_time": 1000.0,
+      "metric_roles": {
+        "circulation_strength_history": "diagnostic",
+        "convection_mean_speed": "principal",
+        "temperature_max": "principal",
+        "temperature_min": "principal",
+        "thermal_vertical_profile": "principal"
+      },
+      "principal_metrics": [
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+            }
+          ]
+        },
+        "shock_feature_locations": {
+          "events": [
+            {
+              "coordinate": 0.12570827189875775,
+              "field": "p",
+              "local_cell_size": 0.01142951678666998,
+              "profile_id": "streamline_0.25"
+            },
+            {
+              "coordinate": 0.2133297635403013,
+              "field": "p",
+              "local_cell_size": 0.011429124055609502,
+              "profile_id": "streamline_0.50"
+            },
+            {
+              "coordinate": 0.27064612304654734,
+              "field": "p",
+              "local_cell_size": 0.011077577496824809,
+              "profile_id": "streamline_0.75"
+            }
+          ],
+          "kind": "profile_feature_locations"
+        },
+        "shock_pressure_jump_ratio": 4.742399934066266,
+        "supersonic_volume_fraction": 1.0
+      },
+      "source_case_id": "wedge/9",
+      "tolerances": {
+        "pressure_mach_profiles": {
+          "criterion_role": "principal_response_shape",
+          "kind": "named_profiles",
+          "normalization_floors": {
+            "Mach": 0.0001,
+            "p": 1.0,
+            "speed": 1e-05,
+            "u": 1e-05
+          },
+          "normalized_l1_max": 0.05,
+          "normalized_linf_max": 0.15,
+          "provisional": true,
+          "reference_independent": false,
+          "threshold_source": "reference_anchored_spatial_response_shape"
+        },
+        "shock_feature_locations": {
+          "kind": "profile_feature_locations",
+          "maximum_cell_offset": 2.0,
+          "physical_floor": 1e-10,
+          "provisional": true
+        },
+        "shock_pressure_jump_ratio": {
+          "criterion_role": "principal_physics",
+          "high": 6.5,
+          "kind": "physics_range",
+          "low": 2.0,
+          "provisional": true,
+          "reference_independent": true,
+          "threshold_source": "bounded_compressive_pressure_feature"
+        },
+        "supersonic_volume_fraction": {
+          "criterion_role": "principal_physics",
+          "high": 1.0,
+          "kind": "physics_range",
+          "low": 0.85,
+          "provisional": true,
+          "reference_independent": true,
+          "threshold_source": "supersonic_regime_coverage_tightened"
+        }
+      },
+      "track": "basic"
+    }
+  },
+  "design": "foambench.basic_advanced.qoi_design",
+  "notes": [
+    "Principal scalar QoIs are reference-independent family physics criteria extracted from retained fields.",
+    "One existing spatial response profile per family is also principal and must jointly pass its reference-anchored shape tolerance.",
+    "Other histories, profiles, and feature locations remain diagnostic and do not decide Physics-grounded pass.",
+    "Provisional physical-signature and response-shape limits require future valid-alternative calibration."
+  ],
+  "openfoam_version": "Foundation v13",
+  "producer": "benchmarks/evaluation/basic_advanced.py",
+  "schema_version": "foambench.reference_qois.v2",
+  "summary": {
+    "case_count": 110,
+    "health_fail_count": 0,
+    "health_pass_count": 110,
+    "tracks": [
+      "basic"
+    ]
+  },
+  "tolerance_policy": "physics_grounded_scalar_and_response_shape_joint_gate.v2"
+}
diff --git a/benchmarks/FoamBench_extended_openfoam13_evidence_contract.v1.json b/benchmarks/FoamBench_extended_openfoam13_evidence_contract.v1.json
new file mode 100644
index 0000000000000000000000000000000000000000..38ab9f4061b4fe125eb65298c28aac3806c1390d
--- /dev/null
+++ b/benchmarks/FoamBench_extended_openfoam13_evidence_contract.v1.json
@@ -0,0 +1,59 @@
+{
+  "schema_version": "foambench.evidence.contract.v1",
+  "purpose": "Agent-independent discovery and validation contract for physics-grounded QoI evidence",
+  "normalization": "lowercase ASCII alphanumeric for routing hints only",
+  "roots": [
+    "case/postProcessing",
+    "case/postprocessing",
+    "case/results",
+    "case/outputs",
+    "workspace/postProcessing",
+    "workspace/postprocessing",
+    "workspace/results",
+    "workspace/outputs",
+    "workspace/evidence",
+    "workspace/reports"
+  ],
+  "manifest": {
+    "path": "workspace/evidence/qoi_manifest.v1.json",
+    "required_fields": ["metric", "path", "kind", "columns", "time_semantics", "method_version"],
+    "path_policy": "path must resolve below a canonical evidence root",
+    "priority": ["validated_manifest", "deterministic_field_derivation", "semantic_discovery"]
+  },
+  "kinds": {
+    "force_coefficients": {
+      "aliases": ["forcecoeffs", "forcecoefficients", "forcecoefficient", "aerodynamicloads", "aeroloads", "loads"],
+      "required_columns": ["Time", "at_least_one_of:Cd,Cl,Cm"],
+      "physical_validation": "coefficient table with declared reference normalization"
+    },
+    "patch_flux": {
+      "aliases": ["patchflowrate", "patchflow", "massflow", "massflux", "rhophi", "fluxhistory"],
+      "required_columns": ["Time", "explicit_mass_or_volumetric_flux"],
+      "physical_validation": "patch identity and phi dimensions/unit declaration"
+    },
+    "patch_pressure": {
+      "aliases": ["patchaverage", "patchintegrate", "pressurerise", "pressuredifference", "patchpressure"],
+      "required_columns": ["Time", "pressure", "inlet_identity", "outlet_identity"],
+      "physical_validation": "static/total pressure convention and outlet-minus-inlet orientation"
+    },
+    "wall_law_profile": {
+      "aliases": ["spaldingcomparison", "uplusyplus", "walllawprofile", "velocityprofile", "wallprofile"],
+      "required_columns": ["y_plus_alias"],
+      "optional_columns": ["u_plus_alias", "spalding_prediction_alias"],
+      "physical_validation": "wall/region identity and final-saved-time or declared profile time"
+    },
+    "centerline_profile": {
+      "aliases": ["centerline", "centreline", "horizontal", "vertical", "px0", "py0", "rhox0", "rhoy0"],
+      "required_columns": ["coordinate", "at_least_one_of:p,rho,U"],
+      "physical_validation": "line orientation and sample time must be recoverable"
+    },
+    "bubble_geometry": {
+      "aliases": ["bubblegeometry", "bubblemetrics", "interfacegeometry"],
+      "required_columns": ["component_identity", "geometry_value"],
+      "physical_validation": "derived from alpha/interface fields; undefined topology is not incomplete evidence"
+    }
+  },
+  "proxy_policy": "A routing hint never promotes a file to evidence; metric-specific content, units, dimensions, identity, and time validation are mandatory.",
+  "unresolved_status": "unresolved_evidence",
+  "extractor_method_version": "physics_grounded_qoi.extractors.v3.1"
+}
diff --git a/benchmarks/FoamBench_extended_openfoam13_fixed.json b/benchmarks/FoamBench_extended_openfoam13_fixed.json
new file mode 100644
index 0000000000000000000000000000000000000000..87ea0832f881941b46a25d317cccdba12335900e
--- /dev/null
+++ b/benchmarks/FoamBench_extended_openfoam13_fixed.json
@@ -0,0 +1,2421 @@
+{
+  "yPlusVerification/1": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 15 wall-normal cells with a grading ratio of 1 and the RAS kOmega turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmega;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   20;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/2": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 15 wall-normal cells with a grading ratio of 1 and the RAS kEpsilon turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   20;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/3": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LaunderSharmaKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           LaunderSharmaKE;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    //hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n    hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n    //hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         2500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/v2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      v2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/f": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      f;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/4": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LamBremhorstKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           LamBremhorstKE;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    //hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n    hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n    //hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         2500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/v2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      v2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/f": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      f;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/5": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LienCubicKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           LienCubicKE;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    //hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n    hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n    //hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         2500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/v2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      v2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/f": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      f;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/6": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS v2f low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           v2f;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    //hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n    hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n    //hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         2500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/v2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      v2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/f": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      f;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/7": {
+    "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS qZeta low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutLowReWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           qZeta;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    //hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n    hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n    //hex (0 1 2 3 4 5 6 7) (1 50 1) simpleGrading (1 100 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         2500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n    div(phi,q)                              bounded Gauss limitedLinear 1;\n    div(phi,zeta)                              bounded Gauss limitedLinear 1;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2|q|zeta)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2|q|zeta)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2|q|zeta)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2|q|zeta)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/zeta": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      zeta;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n\n}\n\n// ************************************************************************* //\n",
+    "0/q": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      q;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform 0.316227766;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n\n}\n\n// ************************************************************************* //\n",
+    "0/v2": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      v2;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.1;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 1e-15;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/f": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      f;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/8": {
+    "usr_requirement": "Perform a steady wall y+ verification in the same 1D periodic channel as yPlusVerification/1 and /2, using foamRun -solver incompressibleFluid, SIMPLE coupling, RAS kOmegaSST, 15 wall-normal cells, uniform grading, nu=2e-5, meanVelocityForce Ubar=(0.4 0 0), endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20. This is the third-model comparison against the kOmega and kEpsilon variants. Take the half-channel height as 1 m.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n    delta           cubeRootVol;\n    filter          simple;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (1 15 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   20;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/9": {
+    "usr_requirement": "Perform the coarse-wall-resolution y+ verification variant with the standard RAS kOmega model on the 30-cell wall-normal mesh with simpleGrading ratio 50. Keep the periodic channel forcing, endTime=500, deltaT=0.25, sampling, and Spalding comparison workflow fixed; this is distinct from the 15-cell kOmega baseline because the mesh and resulting wall-resolution target differ. Take the half-channel height as 1 m. Use kinematic viscosity 2e-5 m2/s and target mean velocity 0.4 m/s.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmega;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (1 30 1) simpleGrading (1 50 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   20;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "yPlusVerification/10": {
+    "usr_requirement": "Perform a wall y+ verification viscosity-sensitivity comparison in a periodic half-channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, steady SIMPLE coupling, a 30-cell wall-normal mesh with grading ratio 50, and RAS kEpsilon. Run three nominal branches labelled Re_tau_180, Re_tau_395, and Re_tau_590 using nu=0.005555555556, 0.002531645570, and 0.001694915254 respectively while keeping meanVelocityForce Ubar=(0.4 0 0), geometry, boundaries, and controls fixed. The labels identify the viscosity values obtained from an initial u_tau=1 estimate; do not assume they are achieved Reynolds numbers. For every converged branch, obtain u_tau from positive computed wall shear, calculate and report achieved Re_tau=u_tau*delta/nu with delta=1, and compare sampled u+ versus y+ against Spalding law. Fail post-processing if wall shear is unavailable. The half-channel height is 1 m; the nominal Reynolds-number labels are only branch names, and the achieved friction Reynolds number must come from the computed wall shear.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0.4 0 0);\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-8;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0001;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            epsilonWallFunction;\n        value           uniform 0.0001;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 1000;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 1000;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    left\n    {\n        type            cyclic;\n    }\n\n    right\n    {\n        type            cyclic;\n    }\n\n    walls\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    centreline\n    {\n        type            symmetryPlane;\n    }\n\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/uniform/time": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"0/uniform\";\n    object      time;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nbeginTime       0;\n\nvalue           0;\n\nname            \"0\";\n\nindex           0;\n\ndeltaT          0.25;\n\ndeltaT0         0.25;\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kEpsilon;\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 2e-5;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 0.1;\n\nvertices\n(\n    (-1  0 -1)\n    ( 1  0 -1)\n    ( 1  10 -1)\n    (-1  10 -1)\n\n    (-1  0  1)\n    ( 1  0  1)\n    ( 1  10  1)\n    (-1  10  1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (1 30 1) simpleGrading (1 50 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    left\n    {\n        type cyclic;\n        neighbourPatch right;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    right\n    {\n        type cyclic;\n        neighbourPatch left;\n        faces\n        (\n            (1 2 6 5)\n        );\n    }\n\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 5 4)\n        );\n    }\n\n    centreline\n    {\n        type symmetryPlane;\n        faces\n        (\n            (2 3 7 6)\n        );\n    }\n\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          0.25;\n\nwriteControl    runTime;\n\nwriteInterval   20;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n//cacheTemporaryObjects\n//(\n//    G\n//);\n\nfunctions\n{\n    yPlus\n    {\n        type yPlus;\n        libs (\"libfieldFunctionObjects.so\");\n        executeControl writeTime;\n        writeControl writeTime;\n    }\n\n    //#includeFunc writeObjects(\"k\")\n\n    //yPlus\n    //{\n    //    libs        (\"libutilityFunctionObjects.so\");\n\n    //    type coded;\n\n    //    codeWrite\n    //    #{\n    //        const volScalarField& R = mesh().lookupObjectRef<volScalarField>(\"R\");\n    //    #};\n    //}\n}\n",
+    "system/fvConstraints": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object fvConstraints;\n}\n\nmomentumForce\n{\n    type meanVelocityForce;\n    cellZone fluid;\n    Ubar (0.4 0 0);\n}\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss linearUpwind grad(U);\n    div(phi,k)      bounded Gauss limitedLinear 1;\n    div(phi,epsilon) bounded Gauss limitedLinear 1;\n    div(phi,omega)  bounded Gauss limitedLinear 1;\n    div(phi,nuTilda) bounded Gauss limitedLinear 1;\n    div(phi,f)      bounded Gauss limitedLinear 1;\n    div(phi,v2)     bounded Gauss limitedLinear 1;\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n    div(nonlinearStress) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon|omega|nuTilda|f|v2)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon|omega|nuTilda|f|v2)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n(\n    data\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 0 0);\n        end     (0 1 0);\n        nPoints 100;\n    }\n);\n\nfields (U yPlus);\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleFluid\"\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\nrunApplication postProcess -solver incompressibleFluid -func yPlus\nrunApplication -a postProcess -latestTime -solver incompressibleFluid -func wallShearStress\nrunApplication -a postProcess -latestTime -func sample\npython3 system/spaldingCompare.py",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    fluidCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-1e10 -1e10 -1e10) (1e10 1e10 1e10);\n    }\n\n    {\n        name    fluid;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     fluidCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "reference_subcases": [
+      {
+        "id": "Re_tau_180",
+        "delta": 1,
+        "nu": 0.005555555555555556,
+        "usr_requirement": "Run the periodic-channel viscosity branch Re_tau_180 with nu=0.005555555555555556, Ubar=(0.4 0 0), delta=1, the 30-cell grading-50 mesh, RAS kEpsilon, and steady SIMPLE controls. Treat 180 as a nominal label only; derive u_tau from computed positive wall shear and report the achieved Re_tau=u_tau/nu. Do not use a hard-coded friction velocity. The half-channel height is 1 m; the nominal Reynolds-number labels are only branch names, and the achieved friction Reynolds number must come from the computed wall shear.",
+        "overrides": {
+          "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 0.005555555556;\n\n// ************************************************************************* //\n",
+          "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nmomentumForce\n{\n    type            meanVelocityForce;\n\n    cellZone        fluid;\n\n    Ubar            (0.4 0 0);\n}\n\n// ************************************************************************* //\n"
+        },
+        "nominal_Re_tau": 180
+      },
+      {
+        "id": "Re_tau_395",
+        "delta": 1,
+        "nu": 0.002531645569620253,
+        "usr_requirement": "Run the periodic-channel viscosity branch Re_tau_395 with nu=0.002531645569620253, Ubar=(0.4 0 0), delta=1, the 30-cell grading-50 mesh, RAS kEpsilon, and steady SIMPLE controls. Treat 395 as a nominal label only; derive u_tau from computed positive wall shear and report the achieved Re_tau=u_tau/nu. Do not use a hard-coded friction velocity. The half-channel height is 1 m; the nominal Reynolds-number labels are only branch names, and the achieved friction Reynolds number must come from the computed wall shear.",
+        "overrides": {
+          "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 0.00253164557;\n\n// ************************************************************************* //\n",
+          "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nmomentumForce\n{\n    type            meanVelocityForce;\n\n    cellZone        fluid;\n\n    Ubar            (0.4 0 0);\n}\n\n// ************************************************************************* //\n"
+        },
+        "nominal_Re_tau": 395
+      },
+      {
+        "id": "Re_tau_590",
+        "delta": 1,
+        "nu": 0.001694915254237288,
+        "usr_requirement": "Run the periodic-channel viscosity branch Re_tau_590 with nu=0.001694915254237288, Ubar=(0.4 0 0), delta=1, the 30-cell grading-50 mesh, RAS kEpsilon, and steady SIMPLE controls. Treat 590 as a nominal label only; derive u_tau from computed positive wall shear and report the achieved Re_tau=u_tau/nu. Do not use a hard-coded friction velocity. The half-channel height is 1 m; the nominal Reynolds-number labels are only branch names, and the achieved friction Reynolds number must come from the computed wall shear.",
+        "overrides": {
+          "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\nnu              [0 2 -1 0 0 0 0] 0.001694915254;\n\n// ************************************************************************* //\n",
+          "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nmomentumForce\n{\n    type            meanVelocityForce;\n\n    cellZone        fluid;\n\n    Ubar            (0.4 0 0);\n}\n\n// ************************************************************************* //\n"
+        },
+        "nominal_Re_tau": 590
+      }
+    ],
+    "system/spaldingCompare.py": "#!/usr/bin/env python3\nimport math\nimport pathlib\nimport re\nimport sys\nif len(sys.argv) > 1:\n    src = pathlib.Path(sys.argv[1])\nelse:\n    candidates = sorted([p for p in pathlib.Path(\"postProcessing\").rglob(\"*\") if p.suffix in {\".raw\", \".xy\"} and \"spalding_comparison\" not in p.name]) if pathlib.Path(\"postProcessing\").exists() else []\n    def time_key(path):\n        try:\n            return float(path.parent.name)\n        except ValueError:\n            return -1.0\n    src = max(candidates, key=time_key) if candidates else pathlib.Path(\"postProcessing/sample/0/data.raw\")\nout = src.with_name(\"spalding_comparison.raw\")\nkap, B = 0.41, 5.2\ntauw = None\nwall_files = sorted(pathlib.Path(\"postProcessing\").rglob(\"wallShearStress.dat\")) if pathlib.Path(\"postProcessing\").exists() else []\nif wall_files:\n    for line in reversed(wall_files[-1].read_text().splitlines()):\n        nums = line.replace(\"(\", \" \").replace(\")\", \" \").split()\n        try:\n            if len(nums) >= 8:\n                tauw = abs(float(nums[2]))\n                break\n        except ValueError:\n            pass\nif tauw is None or tauw <= 0:\n    raise RuntimeError(\"Positive wall shear stress was not found; refusing to fabricate friction velocity\")\nutau = math.sqrt(tauw)\nnu = None\nfor prop in (pathlib.Path(\"constant/physicalProperties\"), pathlib.Path(\"constant/physicalProperties.air\")):\n    if prop.exists():\n        match = re.search(r\"(?m)^\\s*nu\\s+(?:\\[[^]]+\\]\\s+)?([0-9.eE+-]+)\\s*;\", prop.read_text())\n        if match:\n            nu = float(match.group(1))\n            break\nif nu is None or nu <= 0:\n    raise RuntimeError(\"Could not determine positive kinematic viscosity from constant physicalProperties\")\nachieved_re_tau = utau / nu\nprint(f\"u_tau={utau:.12g} nu={nu:.12g} achieved_Re_tau={achieved_re_tau:.12g}\")\nwith out.open(\"w\") as stream:\n    stream.write(\"# yPlus uPlus spaldingYPlus residual\\n\")\n    for line in (src.read_text().splitlines() if src.exists() else []):\n        try:\n            vals = [float(x) for x in line.replace(\"(\", \" \").replace(\")\", \" \").split()]\n        except ValueError:\n            continue\n        if len(vals) < 2:\n            continue\n        yp = utau * vals[0] / nu\n        up = abs(vals[1]) / utau\n        sp = up + math.exp(-kap * B) * (math.exp(kap * up) - 1 - kap * up - (kap * up)**2 / 2 - (kap * up)**3 / 6)\n        stream.write(f\"{yp:.12g} {up:.12g} {sp:.12g} {yp-sp:.12g}\\n\")\n"
+  },
+  "risingBubble/1": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/2": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (40 80 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (40 80 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 40x80 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/3": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (80 160 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (80 160 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 80x160 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/4": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss interfaceCompression linear 1;\n    div(phirb,alpha)                           Gauss interfaceCompression linear 1;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Change only the interface-capturing scheme relative to the vanLeer baseline: use the explicit interfaceCompression alpha-transport scheme with a linear base interpolation instead of the baseline Gauss vanLeer alpha advection. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/5": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss PLIC interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.water.*\"\n    {\n        nCorrectors     2;\n        nSubCycles      1;\n\n        MULESCorr       yes;\n\n        MULES\n        {\n            nIter           10;\n            tolerance       1e-8;\n            globalBounds    true;\n        }\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. This variant follows the PDF design intent of an isoAdvector geometric reconstruction comparison, but OpenFOAM Foundation v13 does not provide the original isoAdvector method in this solver path; implement the closest available geometric VOF analogue as Gauss PLIC interfaceCompression vanLeer 1. Therefore the research purpose is comparable to the isoAdvector variant, while the numerical method entity is the Foundation-v13 PLIC/interfaceCompression approximation rather than native isoAdvector. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/6": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 12.25;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=12.25, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/7": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 49.0;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=49.0, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/8": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 24.5;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n    front\n    {\n        type symmetryPlane;\n        faces\n        (\n            (0 3 2 1)\n        );\n    }\n    back\n    {\n        type symmetryPlane;\n        faces\n        (\n            (4 5 6 7)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Use adaptive mesh refinement with dynamicRefineFvMesh to refine the mesh around the gas-liquid interface during the calculation, while keeping the initial coarse mesh and baseline physical properties; implement the reference case as a thin quasi-2D slab with front/back symmetry planes if needed for OpenFOAM dynamic refinement. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    refineInterval  1;\n\n    field           alpha.water;\n\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    nBufferLayers   1;\n\n    maxRefinement   2;\n\n    maxCells        200000;\n\n    dumpLevel       true;\n}\n\n// ************************************************************************* //\n"
+  },
+  "risingBubble/9": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 6.125;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.01;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=6.125, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. This is the high-Eotvos-number variant, using the lower surface tension as a physically consistent high-Eo parameter set so the bubble deforms more strongly than the baseline rising-bubble case. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "risingBubble/10": {
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    bottom\n    {\n        type            slip;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            slip;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    bottom\n    {\n        type            fixedFluxPressure;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    walls\n    {\n        type            fixedFluxPressure;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    bottom\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    walls\n    {\n        type            zeroGradient;\n    }\n\n    defaultFaces\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           ( 0 -0.98 0 );\n//value           ( 0 0 0 );\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 6.125;\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.1;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 100;\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 0.1;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1000;\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (1 0 0)\n    (1 2 0)\n    (0 2 0)\n    (0 0 0.1)\n    (1 0 0.1)\n    (1 2 0.1)\n    (0 2 0.1)\n);\n\nblocks\n(\n     //hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n     hex (0 1 2 3 4 5 6 7) (20 40 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    bottom\n    {\n        type wall;\n        faces\n        (\n            (1 5 4 0)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (3 7 6 2)\n        );\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 4 7 3)\n            (2 6 5 1)\n        );\n    }\n\n    defaultFaces\n    {\n        type empty;\n        faces\n        (\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         7;\n\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.1;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.5;\nmaxAlphaCo      0.9;\nmaxDeltaT       0.9;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss linearUpwind grad(U);\n    div(phi,alpha)                             Gauss vanLeer;\n    div(phirb,alpha)                           Gauss vanLeer;\n    div(rhoPhi,U)  Gauss linearUpwind grad(U);\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 1;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-7;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-7;\n        relTol          0;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-06;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n);\n\nregions\n(\n    cylinderToCell\n    {\n\t    p1 (0.5 0.8 -1);\n\t    p2 (0.5 0.8 1);\n\t    radius 0.15;\n\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n        );\n    }\n);\n",
+    "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=6.125, water density=1000 kg/m3, air density=100 kg/m3, liquid kinematic viscosity nu=0.1, air kinematic viscosity nu=0.1, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. This is a high-Eotvos-number and high-Morton-number sensitivity variant using lower surface tension and higher viscosity than the baseline, intended to explore a strongly deformed/skirt-bubble regime. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.1 and 0.1 m2/s, respectively.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n"
+  },
+  "supersonicCrossJet/1": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: baseline Ma=2.0 and reference pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/2": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: mainflow Mach number Ma=3.0. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(1203 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (1203 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (1203 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/3": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: low jet-to-mainstream pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=50000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 50000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/4": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: high jet-to-mainstream pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=200000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 200000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/5": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: 30 degree injection angle. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(300.749 173.637 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (300.749 173.637 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/6": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: 60 degree injection angle. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(173.637 300.749 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (173.637 300.749 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/7": {
+    "usr_requirement": "Perform the compressible supersonic jet-in-crossflow benchmark with the same Ma=2, pressure ratio, thermophysical model, solver, and controls as the baseline, but refine the first active mainflow block in the streamwise direction from 40 to 80 cells. Preserve all other blocks, boundaries, and numerical schemes. This is the mesh-resolution variant; the 90-degree injection angle is already represented by the baseline case. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n    hex (0 1 5 4 3 2 6 7) \t      (80 1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (80   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/8": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: unbounded Gauss upwind convection retained for the full steady run, distinct from the bounded-upwind baseline. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,k)          Gauss upwind;\n    div(phi,K)          Gauss upwind;\n    div(phi,Ekp)        Gauss upwind;\n    div(phi,e)          Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          Gauss upwind;\n    div(phi,rho)        Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n"
+  },
+  "supersonicCrossJet/9": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: earlier transition from upwind to bounded limitedLinear 0.05 steady schemes. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. For this staged scheme variant, run system/fvSchemes.upwind from iteration 0 to 300, then continue from latestTime with system/fvSchemes.limitedLinear, using bounded limitedLinear 0.05 convection, to iteration 1000. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\ncp system/fvSchemes.upwind system/fvSchemes\nrunApplication -overwrite foamDictionary -entry startFrom -set startTime system/controlDict\nrunApplication -overwrite foamDictionary -entry endTime -set 300 system/controlDict\nrunApplication -overwrite -suffix upwind foamRun -solver fluid\ncp system/fvSchemes.limitedLinear system/fvSchemes\nrunApplication -overwrite foamDictionary -entry startFrom -set latestTime system/controlDict\nrunApplication -overwrite foamDictionary -entry endTime -set 1000 system/controlDict\nrunApplication -overwrite foamRun -solver fluid\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   250;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n\nsolver           fluid;",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.5;\n    maxFactor  2;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        250;\n    max        800;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss limitedLinearV 0.05;\n    div(phi,epsilon)    bounded Gauss limitedLinear 0.05;\n    div(phi,k)          bounded Gauss limitedLinear 0.05;\n    div(phi,K)          bounded Gauss limitedLinear 0.05;\n    div(phi,Ekp)        bounded Gauss limitedLinear 0.05;\n    div(phi,e)          bounded Gauss limitedLinear 0.05;\n    div(phid,p)         Gauss limitedLinear 0.05;\n    div(phi,(p|rho))    Gauss limitedLinear 0.05;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss limitedLinear 0.05;\n    div(phi,rho)        bounded Gauss limitedLinear 0.05;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-08;\n        relTol          0.01;\n        nCellsInCoarsestLevel 20;\n    }\n\n    \"(U|e|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-08;\n        relTol          0.05;\n    }\n}\n\nSIMPLE\n{\n    nUCorrectors        2;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n    consistent      no;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.05;\n        rho             0.05;\n    }\n    equations\n    {\n        U               0.02;\n        e               0.02;\n        k               0.2;\n        epsilon         0.2;\n    }\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes.upwind": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss upwind;\n    div(phi,epsilon)    bounded Gauss upwind;\n    div(phi,k)          bounded Gauss upwind;\n    div(phi,K)          bounded Gauss upwind;\n    div(phi,Ekp)        bounded Gauss upwind;\n    div(phi,e)          bounded Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss upwind;\n    div(phi,rho)        bounded Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes.limitedLinear": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             steadyState;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          bounded Gauss limitedLinearV 0.05;\n    div(phi,epsilon)    bounded Gauss limitedLinear 0.05;\n    div(phi,k)          bounded Gauss limitedLinear 0.05;\n    div(phi,K)          bounded Gauss limitedLinear 0.05;\n    div(phi,Ekp)        bounded Gauss limitedLinear 0.05;\n    div(phi,e)          bounded Gauss limitedLinear 0.05;\n    div(phid,p)         Gauss limitedLinear 0.05;\n    div(phi,(p|rho))    Gauss limitedLinear 0.05;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          bounded Gauss limitedLinear 0.05;\n    div(phi,rho)        bounded Gauss limitedLinear 0.05;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/stagedRunDict": "FoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      stagedRunDict;\n}\nstages\n(\n    {\n        schemes     fvSchemes.upwind;\n        startFrom   startTime;\n        endTime     300;\n        log         log.rhoSimpleFoam.upwind;\n    }\n    {\n        schemes     fvSchemes.limitedLinear;\n        startFrom   latestTime;\n        endTime     1000;\n        log         log.rhoSimpleFoam;\n    }\n);\n"
+  },
+  "supersonicCrossJet/10": {
+    "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the rhoPimpleFoam-style pseudo-transient solver switch in OpenFOAM-13 via foamRun -solver fluid. Variant: rhoPimpleFoam pseudo-transient solver-family switch relative to the rhoSimpleFoam steady baseline. Keep the Ma=2 physical geometry and inlet states of the baseline. Run a non-smoke transient PIMPLE window from t=0 to t=0.05 with deltaT=2e-6 and write every 0.005 simulation-time units. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\nrunApplication blockMesh\nrunApplication foamRun -solver fluid\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (801.997 0 0);\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform (801.997 0 0);\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform (0 347.275 0);\n    }\n    top\n    {\n        type            slip;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    obstacle\n    {\n        type            slip;\n    }\n    bottom\n    {\n        type            slip;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 100000;\n\nboundaryField\n{\n    inlet1\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    inlet2\n    {\n        type            fixedValue;\n        value           uniform 100000;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            waveTransmissive;\n        field           p;\n        gamma           1.4;\n        fieldInf        100000;\n        lInf            5;\n        value           uniform 100000;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 400;\n\nboundaryField\n{\n    inlet1\n    {\n        type           fixedValue;\n        value          uniform 400;\n    }\n    inlet2\n    {\n        type           fixedValue;\n        value          uniform 300;\n    }\n    top\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 400;\n        value           uniform 400;\n    }\n    obstacle\n    {\n        type            zeroGradient;\n    }\n    bottom\n    {\n        type            zeroGradient;\n    }\n    frontandback\n    {\n        type            empty;\n    }\n}\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              2.544e+06;\n    }\n    transport\n    {\n        mu              1e-5;\n        Pr              1;\n    }\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0  0   1) \t\t//0\n    (2  0   1) \t\t//1\n    (2  0.1 1) \t\t//0\n    (0  0.1 1) \t\t//1\n    \n    (0  0   0) \t\t//0\n    (2  0   0) \t\t//1\n    (2  0.1 0) \t\t//0\n    (0  0.1 0) \t\t//1\n\n    (-3.33333  0.1 0) \t//0\n    (-3.33333  0.1 1) \t//1\n    (-3.33333  0   0) \t//0\n    (-3.33333  0   1) \t//1\n\n    (2    \t1 1)\n    (0    \t1 1)\n    (-3.33333 \t1 1)\n    (-3.33333 \t1 0)\n    (0    \t1 0)\n    (2    \t1 0)\n\n    (-0.05 0.1 0)\n    (-0.05 0.1 1)\n    (-0.05 0 0)\n    (-0.05 0 1)\n    (-0.05 1 0)\n    (-0.05 1 1)\n\n);\n\nblocks\n(\n/*\n    hex (0 1 5 4 3 2 6 7) \t(100 \t1 225) simpleGrading (20 \t1 500)\n    hex (11 0 4 10 9 3 7 8) \t(20 \t1 225) simpleGrading (0.05 \t1 500)\n    hex (9 3 7 8 14 13 16 15) \t(20 \t1  10) simpleGrading (0.05 \t1 20)\n    hex (3 2 6 7 13 12 17 16) \t(100 \t1  10) simpleGrading (20 \t1 20)\n*/\n\n    hex (0 1 5 4 3 2 6 7) \t      (40 \t1 6)  simpleGrading (1 1 1 )\n    hex (11 21 20 10 9 19 18 8)   (80 \t1 6)  simpleGrading (1 1 1 )\n    hex (9 19 18 8 14 23 22 15)   (80 \t1 50)  simpleGrading (1 1 1 )\n    hex (19 3 7 18 23 13 16 22)   (3 \t1 50)  simpleGrading (1 1 1 )\n    hex (3 2 6 7 13 12 17 16)     (40   1 50)    simpleGrading (1 1 1 )\n\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet1\n    {\n        type patch;\n        faces\n        (\n            (9 8 10 11)\n            (14 15 8 9)\n        );\n    }\n    inlet2\n    {\n        type patch;\n        faces\n        (\n           (19 18 7 3)\n        );\n    }\n    top\n    {\n        type patch;\n        faces\n        (\n\t\t(15 14 23 22)\n\t\t(16 13 12 17)\n                (22 23 13 16)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (2 6 17 12)\n        );\n    }\n    \n    bottom\n    {\n        type wall;\n        faces\n        (\n            (0 4 5 1)\n            (11 10 20 21)\n        );\n    }\n    \n    obstacle\n    {\n        type wall;\n        faces\n        (\n           (21 20 18 19)\n           (0 3 7 4)\n        );\n    }\n    frontandback\n    {\n        type empty;\n        faces\n        (\n            (0 1 2 3)\n\t    (5 4 7 6)\n            (11 21 19 9)\n\t    (20 10 8 18)\n            (9 19 23 14)\n\t    (3 2 12 13)\n\t    (6 7 16 17)\n \t    (18 8 15 22)\n            (19 3 13 23)\n            (7 18 22 16)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\nstartTime       0;\nstopAt          endTime;\nendTime         0.05;\ndeltaT          2e-6;\nmaxDeltaT       2e-6;\nmaxCo           0.5;\nadjustTimeStep  no;\nwriteControl    runTime;\nwriteInterval   0.005;\npurgeWrite      0;\nwriteFormat     ascii;\nwritePrecision  6;\nwriteCompression off;\ntimeFormat      general;\ntimePrecision   6;\ngraphFormat     raw;\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\nlimitp\n{\n    type       limitPressure;\n    minFactor  0.1;\n    maxFactor  5;\n}\nlimitt\n{\n    type       limitTemperature;\n    cellZone   all;\n    min        101;\n    max        2000;\n}\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default             Euler;\n}\n\ngradSchemes\n{\n    default             Gauss linear;\n    grad(U)             cellLimited Gauss linear 1;\n    grad(e)             cellLimited Gauss linear 1;\n    grad(p)             cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default             none;\n    div(phi,U)          Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,k)          Gauss upwind;\n    div(phi,K)          Gauss upwind;\n    div(phi,Ekp)        Gauss upwind;\n    div(phi,e)          Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U)))))      Gauss linear;\n    div(phi,p)          Gauss upwind;\n    div(phi,rho)        Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n\nsolvers\n{\n    \"rho.*\"\n    {\n        solver          diagonal;\n    }\n    \"p.*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n    \"(U|e|k|epsilon).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n    nCorrectors      1;\n    nNonOrthogonalCorrectors 0;\n    transonic       no;\n}\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/1": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. CDV baseline transonic case with throat Mach number approximately 1.0. Use this as the reference structured-mesh, laminar, fluid-solver configuration. Keep the CDV geometry, structured 2D mesh, thermophysical model, laminar model, physical flow condition, and pressure-density convection format div(phi,(p|rho)) unchanged unless this variant explicitly changes that one main variable. Run as transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/2": {
+    "usr_requirement": "Perform the CDV baseline compressible nozzle case with foamRun -solver fluid, using the supplied structured CDV geometry and a throat-refined mesh. Change only the first converging-section cell count from 40 to 80 (with all solver, thermophysical, flow, boundary, and run settings unchanged); this is the mesh-resolution variant. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (80 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/3": {
+    "usr_requirement": "Perform the supplied CDV compressible nozzle case with foamRun -solver fluid at a reduced outlet back pressure of 95000 Pa. Keep the CDV geometry, mesh, solver, thermophysical model, inlet state, discretisation, and run controls fixed; this is the back-pressure variant distinct from the mesh-refined nozzleCDV/2 case. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 95000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 95000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/4": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Back-pressure scan for subsonic, transonic, and supersonic CDV response. Change only the outlet static pressure by running three otherwise identical subcases with pBack=101325, 90000, and 35000 Pa; keep inlet velocity, geometry, mesh, solver, turbulence model, and schemes fixed. Run each subcase from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. For every branch use a 300 K inlet and the 320 m/s baseline inlet speed; vary only the outlet pressure values stated above. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nfor pBack in 101325 90000 35000\ndo\n    caseDir=\"pBack_${pBack}\"\n    mkdir -p \"$caseDir\"\n    cp -r 0 constant system \"$caseDir\"/\n    (\n        cd \"$caseDir\" || exit 1\n        runApplication -s internalPressure foamDictionary -entry internalField -set \"uniform $pBack\" 0/p\n        runApplication -s outletPressure foamDictionary -entry boundaryField/outlet/value -set \"uniform $pBack\" 0/p\n        runApplication blockMesh\n        runApplication foamRun -solver $solver\n    ) || exit 1\ndone\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (p);\n\nsets\n(\n    linex\n    {\n        type        lineUniform;\n        axis        x;\n        start       (0 0 0.005);\n        end         (1 0 0.005);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/5": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Mesh-type variant for the design-table comparison between the structured blockMesh baseline and a non-structured/polyhedral mesh. Change only the mesh representation by starting from the same CDV blockMesh geometry and converting the hex mesh with polyDualMesh using featureAngle=70; keep the geometry envelope, solver, laminar model, target flow condition, boundary conditions, and numerical schemes otherwise fixed. Run transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Compare this case against nozzleCDV/1 as the structured-mesh reference. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication polyDualMesh 70 -overwrite\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/polyDualMeshDict": "featureAngle 70;\n"
+  },
+  "nozzleCDV/6": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Discretisation-format variant from the design table: run an upwind stabilisation stage first, then switch to the stable higher-order linear/limited convection treatment used by the baseline for the remaining time. Change only the convection discretisation by running with system/fvSchemes.upwind to t=0.0025 and then continuing from latestTime with system/fvSchemes.limitedLinear to t=0.005; keep geometry, mesh, solver, laminar model, flow target, and boundary conditions fixed. Write results every 0.001 simulation-time units. Use distinct upwind and limitedLinear log suffixes so the second stage is executed rather than skipped by RunFunctions. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\ncp system/fvSchemes.upwind system/fvSchemes\nrunApplication foamDictionary -entry endTime -set 0.0025 system/controlDict\nrunApplication -s upwind foamRun -solver $solver\ncp system/fvSchemes.limitedLinear system/fvSchemes\nrunApplication foamDictionary -entry startFrom -set latestTime system/controlDict\nrunApplication foamDictionary -entry endTime -set 0.005 system/controlDict\nrunApplication -s limitedLinear foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes.limitedLinear": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSchemes.upwind": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss upwind;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/7": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Boundary-condition variant from the design table using total pressure and total temperature at the inlet with a static-pressure outlet. Change only the inlet/outlet boundary-condition formulation; keep the CDV geometry, structured 2D mesh, solver, laminar model, target flow condition, and numerical schemes fixed. Run transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use inlet total pressure 350000 Pa and total temperature 300 K, with a 90000 Pa static-pressure outlet. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            totalPressure;\n        p0              uniform 350000;\n        gamma           1.4;\n        value           uniform 90000;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            totalTemperature;\n        T0              uniform 300;\n        gamma           1.4;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/8": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver shockFluid. Solver-comparison variant using shockFluid, the OpenFOAM-13 replacement for the legacy rhoCentralFoam central-upwind shock-capturing solver. Change only the solver family and its required convection schemes; keep geometry, mesh, target inlet speed, inlet thermodynamic state, wall treatment, and turbulence model fixed while using shockFluid-compatible outlet extrapolation. Keep the CDV geometry, structured 2D mesh, thermophysical model, laminar model, physical flow condition, and pressure-density convection format div(phi,(p|rho)) unchanged unless this variant explicitly changes that one main variable. Run as transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-7; write results every 0.001 simulation-time units using a fixed-step shockFluid configuration aligned with the tutorial-style solver setup. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and the 90000 Pa baseline pressure level, with shock-compatible extrapolation at the outlet. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"shockFluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          shockFluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-7;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\nmaxCo           1;\nmaxDeltaT       1e-7;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n\n    reconstruct(rho) vanLeer;\n    reconstruct(U)  vanLeerV;\n    reconstruct(T)  vanLeer;\n\n    flux(rhoU)      linear;\n    interpolate((rho*nuEff)) linear;\n    dotInterpolate(Sf,dev2(T(grad(U)))) linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform (320 0 0);\n        value           uniform (320 0 0);\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 300;\n        value           uniform 300;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/9": {
+    "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Dimension variant from the design table: use a true 2D axisymmetric CDV nozzle simplification represented by a small-angle wedge mesh, not a planar half-channel symmetry-plane approximation. Preserve the axial converging-diverging radius profile, collapse the centerline to an axis patch with empty field conditions, and use front/back wedge patches so the OpenFOAM wedge formulation includes the cylindrical-coordinate geometric effect. Use a standard compressible nozzle boundary-condition formulation with totalPressure p0=160000 Pa and totalTemperature T0=300 K at the inlet, pressureInletOutletVelocity for the open velocity boundaries, and a static-pressure outlet p=90000 Pa. Use slip walls for the inviscid/laminar axisymmetric nozzle-wall idealisation. Run transient PIMPLE pseudo-time integration to a quasi-steady converged state from t=0 to t=0.1 with fixed deltaT=1e-5, adjustTimeStep=no, maxCo=0.5, maxDeltaT=1e-5, and writeInterval=0.02. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use the axisymmetric wedge interpretation and the total-pressure/total-temperature and back-pressure values already stated above.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    location        \"system\";\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.1;\n\ndeltaT          1e-05;\n\nwriteControl    runTime;\n\nwriteInterval   0.02;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  no;\n\nmaxCo           0.5;\n\nmaxDeltaT       1e-05;\n\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss vanAlbada;\n    div(phi,e)          Gauss vanAlbada;\n    div(phi,h)          Gauss vanAlbada;\n    div(phi,T)          Gauss vanAlbada;\n    div(phi,K)          Gauss vanAlbada;\n    div(phi,(p|rho))    Gauss vanAlbada;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n\nconvertToMeters 1;\n\n// 5-degree axisymmetric wedge around the x-axis.\n// Radius profile matches the 2D CDV nozzle: 0.20 -> 0.08 -> 0.08 -> 0.20.\nvertices\n(\n    (0.0 0 0)\n    (0.4 0 0)\n    (0.6 0 0)\n    (1.0 0 0)\n\n    (0.0 0.1998096443 -0.00872387747)\n    (0.4 0.07992385773 -0.00348955099)\n    (0.6 0.07992385773 -0.00348955099)\n    (1.0 0.1998096443 -0.00872387747)\n\n    (0.0 0.1998096443 0.00872387747)\n    (0.4 0.07992385773 0.00348955099)\n    (0.6 0.07992385773 0.00348955099)\n    (1.0 0.1998096443 0.00872387747)\n);\n\nblocks\n(\n    hex (0 1 5 4 0 1 9 8) (40 8 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 1 2 10 9) (20 8 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 2 3 11 10) (40 8 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 1 1 0)\n            (1 2 2 1)\n            (2 3 3 2)\n        );\n    }\n    inlet\n    {\n        type patch;\n        faces ((0 0 8 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 11 3));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (4 8 9 5)\n            (5 9 10 6)\n            (6 10 11 7)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n\ndimensions      [0 1 -1 0 0 0 0];\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n    axis { type empty; }\n    walls { type slip; }\n    front { type wedge; }\n    back { type wedge; }\n}\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n\ndimensions      [1 -1 -2 0 0 0 0];\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            totalPressure;\n        p0              uniform 160000;\n        gamma           1.4;\n        value           uniform 160000;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    axis { type empty; }\n    walls { type zeroGradient; }\n    front { type wedge; }\n    back { type wedge; }\n}\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n\ndimensions      [0 0 0 1 0 0 0];\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            totalTemperature;\n        T0              uniform 300;\n        gamma           1.4;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform 300;\n        value           uniform 300;\n    }\n    axis { type empty; }\n    walls { type zeroGradient; }\n    front { type wedge; }\n    back { type wedge; }\n}\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    axis\n    {\n        type            empty;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n}\n\n\n// ************************************************************************* //\n"
+  },
+  "nozzleCDV/10": {
+    "usr_requirement": "Perform a steady 2D compressible CDV nozzle turbulence comparison using foamRun -solver fluid with RAS kOmegaSST. Keep the supplied structured CDV mesh, thermophysical model, boundary conditions, endTime=0.005, deltaT=1e-6, and sampling fixed; this is the 2D RANS turbulence variant, replacing the physically unsuitable quasi-2D DDES design. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"fluid\"\n\nrunApplication blockMesh\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\nturbulence      on;\n    delta           cubeRootVol;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff  1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.005;\n\ndeltaT          1e-6;\n\nwriteControl    runTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss upwind;\n    div(phid,p)         Gauss upwind;\n    div(phi,e)          Gauss upwind;\n    div(phi,h)          Gauss upwind;\n    div(phi,T)          Gauss upwind;\n    div(phi,K)          Gauss upwind;\n    div(phi,(p|rho))    Gauss upwind;\n    div(phi,k)          Gauss upwind;\n    div(phi,omega)      Gauss upwind;\n    div(phi,epsilon)    Gauss upwind;\n    div(phi,nuTilda)    Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(p|U|e|h|T|k|omega|epsilon|nuTilda).*\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-12;\n        relTol          0;\n    }\n\n    \"rho.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-12;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors     2;\n    nCorrectors          1;\n    nNonOrthogonalCorrectors 0;\n\n    transonic            yes;\n}\n\n// ************************************************************************* //\n",
+    "system/samples": "/*--------------------------------*- C++ -*----------------------------------*/\n\ntype                sets;\ninterpolationScheme cellPoint;\nsetFormat           raw;\n\nwriteControl        writeTime;\n\nfields              (Ma);\n\nsets\n(\n    linex\n    {\n        type        lineCell;\n        axis        x;\n        start       (0  0.001 1);\n        end         (10 0.001 1);\n        nPoints     100;\n    }\n);\n\n\n// *********************************************************************** //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0.0 -0.20 0) (0.4 -0.08 0) (0.6 -0.08 0) (1.0 -0.20 0)\n    (0.0  0.20 0) (0.4  0.08 0) (0.6  0.08 0) (1.0  0.20 0)\n    (0.0 -0.20 0.01) (0.4 -0.08 0.01) (0.6 -0.08 0.01) (1.0 -0.20 0.01)\n    (0.0  0.20 0.01) (0.4  0.08 0.01) (0.6  0.08 0.01) (1.0  0.20 0.01)\n);\n\nblocks\n(\n    hex (0 1 5 4 8 9 13 12) (40 16 1) simpleGrading (1 1 1)\n    hex (1 2 6 5 9 10 14 13) (20 16 1) simpleGrading (1 1 1)\n    hex (2 3 7 6 10 11 15 14) (40 16 1) simpleGrading (1 1 1)\n);\n\nedges\n(\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces ((0 8 12 4));\n    }\n    outlet\n    {\n        type patch;\n        faces ((3 7 15 11));\n    }\n    walls\n    {\n        type wall;\n        faces\n        (\n            (0 1 9 8)\n            (1 2 10 9)\n            (2 3 11 10)\n            (4 12 13 5)\n            (5 13 14 6)\n            (6 14 15 7)\n        );\n    }\n    frontAndBack\n    {\n        type empty;\n        faces\n        (\n            (0 4 5 1)\n            (1 5 6 2)\n            (2 6 7 3)\n            (8 9 13 12)\n            (9 10 14 13)\n            (10 11 15 14)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (320 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform (320 0 0);\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            noSlip;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 90000;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n    outlet\n    {\n        type            fixedValue;\n        value           uniform 90000;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            zeroGradient;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       28.9;\n    }\n    thermodynamics\n    {\n        Cp              1005;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.8e-5;\n        Pr              0.7;\n    }\n}\n",
+    "0/Ma": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      Ma;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0.920215;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    outlet\n    {\n        type            calculated;\n        value           uniform 0.920215;\n    }\n    walls\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\ninternalField   uniform 0;\nboundaryField\n{\n    inlet { type calculated; value uniform 0; }\n    outlet { type calculated; value uniform 0; }\n    walls { type compressible::alphatWallFunction; Prt 0.85; value uniform 0; }\n    frontAndBack { type empty; }\n}\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\ninternalField   uniform 1e-5;\nboundaryField\n{\n    inlet { type fixedValue; value uniform 1e-5; }\n    outlet { type zeroGradient; }\n    walls { type fixedValue; value uniform 0; }\n    frontAndBack { type empty; }\n}\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\ninternalField   uniform 0;\nboundaryField\n{\n    inlet { type calculated; value uniform 0; }\n    outlet { type calculated; value uniform 0; }\n    walls { type nutUSpaldingWallFunction; value uniform 0; }\n    frontAndBack { type empty; }\n}\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 1e-5;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 1e-5;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            kqRWallFunction;\n        value           uniform 1e-5;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 100;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform 100;\n    }\n    outlet\n    {\n        type            zeroGradient;\n    }\n    walls\n    {\n        type            omegaWallFunction;\n        value           uniform 100;\n    }\n    frontAndBack\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "MRF_stirredReactor/1": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible laminar stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use a tutorial-derived Rushton stirred tank setup with the tank, shaft, impeller/stirrer, rotating zone, and stationary baffles where applicable. Configure a rotating MRF cellZone for the impeller region at 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and laminar momentum transport. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Include stirrer torque or power monitoring when supported by the tutorial-derived setup. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/2": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible turbulent stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone for the impeller region and stationary tank/baffle walls. Set the impeller speed to 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Include stirrer torque or power monitoring when supported by the tutorial-derived setup. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/3": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible turbulent stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use the same tutorial-derived Rushton stirred tank geometry and rotating MRF cellZone as the kEpsilon baseline. Set the impeller speed to 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and the RAS kOmegaSST turbulence model. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Keep the mesh, boundary conditions, and MRF rotating-zone setup consistent with the kEpsilon case so the turbulence-model effect can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/4": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible stirred-reactor MRF speed-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone and stationary tank/baffle walls. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run an impeller-speed comparison for 50 rpm, 100 rpm, and 200 rpm by changing the rotating-zone omega value while keeping the mesh, boundary conditions, and numerical schemes fixed. Run each speed case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ],
+    "reference_subcases": [
+      {
+        "id": "rpm50",
+        "usr_requirement": "Perform an incompressible stirred-reactor MRF speed-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone and stationary tank/baffle walls. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run an impeller-speed comparison for 50 rpm, 100 rpm, and 200 rpm by changing the rotating-zone omega value while keeping the mesh, boundary conditions, and numerical schemes fixed. Run each speed case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. This reference subcase uses 50 rpm. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     50 [rpm];\n\n// ************************************************************************* //\n"
+        }
+      },
+      {
+        "id": "rpm100",
+        "usr_requirement": "Perform an incompressible stirred-reactor MRF speed-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone and stationary tank/baffle walls. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run an impeller-speed comparison for 50 rpm, 100 rpm, and 200 rpm by changing the rotating-zone omega value while keeping the mesh, boundary conditions, and numerical schemes fixed. Run each speed case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. This reference subcase uses 100 rpm. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n"
+        }
+      },
+      {
+        "id": "rpm200",
+        "usr_requirement": "Perform an incompressible stirred-reactor MRF speed-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone and stationary tank/baffle walls. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run an impeller-speed comparison for 50 rpm, 100 rpm, and 200 rpm by changing the rotating-zone omega value while keeping the mesh, boundary conditions, and numerical schemes fixed. Run each speed case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. This reference subcase uses 200 rpm. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     200 [rpm];\n\n// ************************************************************************* //\n"
+        }
+      }
+    ]
+  },
+  "MRF_stirredReactor/5": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible stirred-reactor MRF baffle-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank setup and compare a baffled tank configuration with four stationary baffles against an otherwise identical unbaffled tank configuration. Use the same rotating MRF cellZone, impeller geometry, Newtonian constant-viscosity fluid, 100 rpm impeller speed, and RAS kEpsilon turbulence model in both configurations. Run each case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps so the baffle effect on flow and stirrer power can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ],
+    "reference_subcases": [
+      {
+        "id": "baffled",
+        "usr_requirement": "Perform an incompressible stirred-reactor MRF baffle-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank setup and compare a baffled tank configuration with four stationary baffles against an otherwise identical unbaffled tank configuration. Use the same rotating MRF cellZone, impeller geometry, Newtonian constant-viscosity fluid, 100 rpm impeller speed, and RAS kEpsilon turbulence model in both configurations. Run each case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps so the baffle effect on flow and stirrer power can be compared. This reference subcase includes four stationary baffles. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n"
+        }
+      },
+      {
+        "id": "unbaffled",
+        "usr_requirement": "Perform an incompressible stirred-reactor MRF baffle-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank setup and compare a baffled tank configuration with four stationary baffles against an otherwise identical unbaffled tank configuration. Use the same rotating MRF cellZone, impeller geometry, Newtonian constant-viscosity fluid, 100 rpm impeller speed, and RAS kEpsilon turbulence model in both configurations. Run each case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps so the baffle effect on flow and stirrer power can be compared. This reference subcase omits the stationary baffles. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "system/createBafflesDict.baffles": ""
+        }
+      }
+    ]
+  },
+  "MRF_stirredReactor/6": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType laminar;\n\nlaminar\n{\n    model               generalisedNewtonian;\n    viscosityModel      CrossPowerLaw;\n\n    nuInf               10;\n    m                   0.4;\n    n                   3;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n    viscosityModel  constant;\n\n    nu              0.01;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform an incompressible stirred-reactor MRF benchmark for a polymer-like non-Newtonian liquid using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use the tutorial-derived Rushton stirred tank geometry with the rotating MRF cellZone, impeller, shaft, and baffles. Configure a generalised-Newtonian CrossPowerLaw viscosity model for the liquid instead of a constant-viscosity Newtonian model. Use an impeller speed of 100 rpm and a steady simpleFoam-style MRF formulation. Run from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Keep the mesh and boundary conditions consistent with the Newtonian MRF baseline so the rheology effect can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. For the non-Newtonian variant use the Cross-Power-Law values nu0=0.01 m2/s, nuInf=10 m2/s, m=0.4 s and n=3. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/7": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   10;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    correctPhi        yes;\n    correctMeshPhi    yes;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform a stirred-reactor comparison between a steady MRF approximation and a sliding-mesh/NCC rotating-impeller calculation using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use tutorial-derived Rushton stirred tank setups for both cases, keeping the tank, baffles, impeller geometry, fluid properties, turbulence model, and impeller speed consistent. For the MRF case, use the rotating MRF cellZone formulation. For the sliding-mesh case, use the corresponding non-conformal coupling or dynamic-mesh tutorial workflow for the rotating impeller region. Use a Newtonian fluid, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Compare the resulting flow field and stirrer power or torque outputs. Extend the full run to t=100 with writeInterval=10 so the sliding-mesh power reaches a stable endpoint. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ],
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Disable motion for an MRF simulation\n// Enable motion for an NCC simulation by changing 'mover-disabled' to 'mover'\nmover\n{\n    type            motionSolver;\n\n    libs            (\"libfvMotionSolvers.so\");\n\n    motionSolver    solidBody;\n\n    cellZone        rotatingZone;\n\n    solidBodyMotionFunction  rotatingMotion;\n\n    #include        \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.NCC": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nfields true;\n\nbaffles\n{\n    nonCouple\n    {\n        type        faceZone;\n        zoneName    rotatingZone;\n\n        owner\n        {\n            name        nonCouple1;\n            type        patch;\n\n            patchFields\n            {\n                #include    \"nonCouplePatchFields\"\n            }\n        }\n\n        neighbour\n        {\n            name        nonCouple2;\n            type        patch;\n\n            patchFields\n            {\n                #include    \"nonCouplePatchFields\"\n            }\n        }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/nonCouplePatchFields": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      nonCouplePatchFields;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nU\n{\n    type            movingWallSlipVelocity;\n    value           uniform (0 0 0);\n}\n\nnut\n{\n    type            calculated;\n    value           uniform 0;\n}\n\n\"(p|k|omega|epsilon)\"\n{\n    type            zeroGradient;\n}\n\n// ************************************************************************* //\n",
+    "reference_subcases": [
+      {
+        "id": "steady_MRF",
+        "usr_requirement": "Perform a stirred-reactor comparison between a steady MRF approximation and a sliding-mesh/NCC rotating-impeller calculation using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use tutorial-derived Rushton stirred tank setups for both cases, keeping the tank, baffles, impeller geometry, fluid properties, turbulence model, and impeller speed consistent. For the MRF case, use the rotating MRF cellZone formulation. For the sliding-mesh case, use the corresponding non-conformal coupling or dynamic-mesh tutorial workflow for the rotating impeller region. Use a Newtonian fluid, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Compare the resulting flow field and stirrer power or torque outputs. This reference subcase uses the steady MRF approximation. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+          "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+          "constant/dynamicMeshDict": "",
+          "system/createBafflesDict.NCC": ""
+        }
+      },
+      {
+        "id": "sliding_mesh_NCC",
+        "usr_requirement": "Perform a stirred-reactor comparison between a steady MRF approximation and a sliding-mesh/NCC rotating-impeller calculation using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use tutorial-derived Rushton stirred tank setups for both cases, keeping the tank, baffles, impeller geometry, fluid properties, turbulence model, and impeller speed consistent. For the MRF case, use the rotating MRF cellZone formulation. For the sliding-mesh case, use the corresponding non-conformal coupling or dynamic-mesh tutorial workflow for the rotating impeller region. Use a Newtonian fluid, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Compare the resulting flow field and stirrer power or torque outputs. This reference subcase uses the sliding-mesh/NCC workflow. Use transient Euler time discretisation with endTime=1, deltaT=0.001, and writeInterval=100 for the moving-mesh branch. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+        "overrides": {
+          "constant/MRFProperties": "",
+          "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// Disable motion for an MRF simulation\n// Enable motion for an NCC simulation by changing 'mover-disabled' to 'mover'\nmover\n{\n    type            motionSolver;\n\n    libs            (\"libfvMotionSolvers.so\");\n\n    motionSolver    solidBody;\n\n    cellZone        rotatingZone;\n\n    solidBodyMotionFunction  rotatingMotion;\n\n    #include        \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+          "system/createBafflesDict.NCC": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nfields true;\n\nbaffles\n{\n    nonCouple\n    {\n        type        faceZone;\n        zoneName    rotatingZone;\n\n        owner\n        {\n            name        nonCouple1;\n            type        patch;\n\n            patchFields\n            {\n                #include    \"nonCouplePatchFields\"\n            }\n        }\n\n        neighbour\n        {\n            name        nonCouple2;\n            type        patch;\n\n            patchFields\n            {\n                #include    \"nonCouplePatchFields\"\n            }\n        }\n    }\n}\n\n// ************************************************************************* //\n",
+          "system/nonCouplePatchFields": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      nonCouplePatchFields;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nU\n{\n    type            movingWallSlipVelocity;\n    value           uniform (0 0 0);\n}\n\nnut\n{\n    type            calculated;\n    value           uniform 0;\n}\n\n\"(p|k|omega|epsilon)\"\n{\n    type            zeroGradient;\n}\n\n// ************************************************************************* //\n",
+          "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    correctPhi        yes;\n    correctMeshPhi    yes;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\" 1;\n    }\n}\n\n// ************************************************************************* //\n",
+          "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            movingWallVelocity;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+          "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+          "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+          "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+          "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+          "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+          "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1;\n\ndeltaT          0.001;\n\nwriteControl    timeStep;\n\nwriteInterval   100;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n"
+        }
+      }
+    ]
+  },
+  "MRF_stirredReactor/8": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor 2;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\ndeltaT          1;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linear;\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform a steady incompressible stirred-reactor MRF mesh-refinement benchmark using foamRun -solver incompressibleFluid with RAS kEpsilon, 100 rpm, the same Rushton geometry, baffles, fluid properties, steady controls, power functions, and boundary conditions as the baseline. Change only the structured tank mesh factor from 1 to 2. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/9": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication mirrorMesh\nfoamDictionary -set \"pointAndNormalDict/normal=(1 0 0)\" system/mirrorMeshDict\nrunApplication -a mirrorMesh\nrunApplication -a createZones\nrunApplication -a createBaffles -dict createBafflesDict.stirrer\nif [ -f system/createBafflesDict.baffles ]; then\n    runApplication -a createBaffles -dict createBafflesDict.baffles\nfi\nif [ -f system/createBafflesDict.NCC ]; then\n    runApplication -a createBaffles -dict createBafflesDict.NCC\n    runApplication splitBaffles\n    runApplication createNonConformalCouples -fields nonCouple1 nonCouple2\nfi\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          1e-3;\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            flowRateInletVelocity;\n        meanVelocity    constant $Uinlet;\n        value           uniform (0 0 0);\n    }\n\n    outlet\n    {\n        type            pressureInletOutletVelocity;\n        value           uniform (0 0 0);\n    }\n\n    stirrer\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            movingWallSlipVelocity;\n        value           uniform (0 0 0);\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            entrainmentPressure;\n        p0              uniform 0;\n        value           uniform 0;\n    }\n\n    stirrer\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    wall\n    {\n        type            fixedFluxExtrapolatedPressure;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-5;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    2e-7;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      0.1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           $internalField;\n    }\n\n    \"nonCouple.*\"\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotatingZone;\n\n    #include \"rotatingZoneProperties\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n    printCoeffs         on;\n}\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu 1e-06;\n\n// ************************************************************************* //\n",
+    "constant/rotatingZoneProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      rotatingZoneProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\norigin    (0 0 0);\naxis      (0 0 1);\nomega     100 [rpm];\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfactor  1;\nmode    uniform;\n\n// Cells\n// multiple of 6, so  mesh faces coincide with six-blade stirrer\nboxCells  #calc \"$factor*6\";\n\nr1Cells   #calc \"$factor*3\";\nr2Cells   $r1Cells;\nr3Cells   $r1Cells;\nr4Cells   #calc \"$factor*4\";\n\n#ifeq $mode graded\n    r5Cells   #calc \"$factor*40\";\n    zCells    #calc \"$factor*100\";\n#else\n    r5Cells   #calc \"$factor*25\";\n    zCells    #calc \"$factor*40\";\n#endif\n\n// Tank\nD       1.0;\nH       1.2;\nR       #calc \"0.5*$D\";\n\n// Rushton radius\nr       #calc \"0.3*$R\";\n\n// Blades\nrbld    #calc \"0.5*$r\";\nrdisk   #calc \"1.5*$rbld\";\nrzone   #calc \"0.4*$R\";\n\n// Box\nrbox    #calc \"0.5*$rbld\";\n\n// 45 degs\nrsqrt2  #calc \"1.0 / sqrt(2.0)\";\n\nrbld45  #calc \"$rsqrt2*$rbld\";\nrdisk45 #calc \"$rsqrt2*$rdisk\";\nr45     #calc \"$rsqrt2*$r\";\nrzone45 #calc \"$rsqrt2*$rzone\";\nR45     #calc \"$rsqrt2*$R\";\n\nconvertToMeters 1;\n\nvertices\n(\n    (0        0        0)\n    ($rbox    0        0)\n    ($rbld    0        0)\n    ($rdisk   0        0)\n    ($r       0        0)\n    ($rzone   0        0)\n    ($R       0        0)\n    (0        $rbox    0)\n    ($rbox    $rbox    0)\n    (0        $rbld    0)\n    ($rbld45  $rbld45  0)\n    (0        $rdisk   0)\n    ($rdisk45 $rdisk45 0)\n    (0        $r       0)\n    ($r45     $r45     0)\n    (0        $rzone   0)\n    ($rzone45 $rzone45 0)\n    (0        $R       0)\n    ($R45     $R45     0)\n\n    (0        0        $H)\n    ($rbox    0        $H)\n    ($rbld    0        $H)\n    ($rdisk   0        $H)\n    ($r       0        $H)\n    ($rzone   0        $H)\n    ($R       0        $H)\n    (0        $rbox    $H)\n    ($rbox    $rbox    $H)\n    (0        $rbld    $H)\n    ($rbld45  $rbld45  $H)\n    (0        $rdisk   $H)\n    ($rdisk45 $rdisk45 $H)\n    (0        $r       $H)\n    ($r45     $r45     $H)\n    (0        $rzone   $H)\n    ($rzone45 $rzone45 $H)\n    (0        $R       $H)\n    ($R45     $R45     $H)\n);\n\n// Grading\n#ifeq $mode graded\n    zGrd   ((1 1 40)(20 4 1)(1 1 0.025));\n    rGrd   ((4 1 1)(1 1 0.025));\n#else\n    zGrd 1;\n    rGrd 1;\n#endif\n\nboxGrd simpleGrading (1 1 $zGrd);\nr1Grd  simpleGrading (1 1 $zGrd);\nr2Grd  simpleGrading (1 1 $zGrd);\nr3Grd  simpleGrading (1 1 $zGrd);\nr4Grd  simpleGrading (1 1 $zGrd);\nr5Grd  simpleGrading ($rGrd 1 $zGrd);\n\nblocks\n(\n    hex (0 1 8 7 19 20 27 26)     ($boxCells $boxCells $zCells) $boxGrd\n\n    hex (1 2 10 8 20 21 29 27)    ($r1Cells $boxCells $zCells) $r1Grd\n    hex (8 10 9 7 27 29 28 26)    ($r1Cells $boxCells $zCells) $r1Grd\n\n    hex (2 3 12 10 21 22 31 29)   ($r2Cells $boxCells $zCells) $r2Grd\n    hex (10 12 11 9 29 31 30 28)  ($r2Cells $boxCells $zCells) $r2Grd\n\n    hex (3 4 14 12 22 23 33 31)   ($r3Cells $boxCells $zCells) $r3Grd\n    hex (12 14 13 11 31 33 32 30) ($r3Cells $boxCells $zCells) $r3Grd\n\n    hex (4 5 16 14 23 24 35 33)   ($r4Cells $boxCells $zCells) $r4Grd\n    hex (14 16 15 13 33 35 34 32) ($r4Cells $boxCells $zCells) $r4Grd\n\n    hex (5 6 18 16 24 25 37 35)   ($r5Cells $boxCells $zCells) $r5Grd\n    hex (16 18 17 15 35 37 36 34) ($r5Cells $boxCells $zCells) $r5Grd\n);\n\ncurve 45 (0 0 1);\n\nedges\n(\n    // Stirrer disk and blades\n    arc 2 10 $curve\n    arc 10 9 $curve\n    arc 21 29 $curve\n    arc 29 28 $curve\n\n    arc 3 12 $curve\n    arc 12 11 $curve\n    arc 22 31 $curve\n    arc 31 30 $curve\n\n    arc 4 14 $curve\n    arc 14 13 $curve\n    arc 23 33 $curve\n    arc 33 32 $curve\n\n    arc 5 16 $curve\n    arc 16 15 $curve\n    arc 24 35 $curve\n    arc 35 34 $curve\n\n    // Outer wall\n    arc 6 18 $curve\n    arc 18 17 $curve\n    arc 25 37 $curve\n    arc 37 36 $curve\n);\n\ndefaultPatch\n{\n    name tank;\n    type wall;\n}\n\n// Optional inlet and outlet patches\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 1 8 7)\n        );\n    }\n    outlet\n    {\n        type patch;\n        faces\n        (\n            (19 26 27 20)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1;\ndeltaT          0.001;\nwriteControl    timeStep;\nwriteInterval   100;\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.baffles": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    bafflesGroup // group name\n    {\n        type        faceZone;\n        zoneName    baffles;\n\n        owner\n        {\n            name        baffles;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createBafflesDict.stirrer": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createBafflesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ninternalFacesOnly true;\n\nbaffles\n{\n    stirrerGroup // not \"stirrer\" otherwise clash between group and patch names\n    {\n        type        faceZone;\n        zoneName    stirrer;\n\n        owner\n        {\n            name        stirrer;\n            type        wall;\n        }\n        neighbour\n        {\n            $owner;\n        }\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/createZonesDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      createZonesDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nstirrer\n{\n    type        union;\n\n    blades\n    {\n        type        surface;\n        surface     triSurface;\n        file        \"stirrer4.obj\";\n    }\n\n    disk\n    {\n        type        surface;\n        surface     disk;\n        origin      (0 0 0.6);\n        normal      (0 0 1);\n        radius      0.1125;\n    }\n}\n\nbaffles\n{\n    type        surface;\n    surface     triSurface;\n    file        \"baffles.obj\";\n}\n\nrotatingZone\n{\n    type        surface;\n    surface     cylinder;\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\nrotatingCellZone\n{\n    type        cylinder;\n    zoneType    cell;\n    name        rotatingZone;\n\n    point1      (0 0 0.54);\n    point2      (0 0 0.66);\n    radius      0.2;\n}\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc power\n#includeFunc stirrerPower\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         Gauss linear;\n    div(phi,U)      Gauss linearUpwind grad(U);\n\n    turbulence      Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon)  $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    \"pcorr.*\"\n    {\n        $p;\n        tolerance       1e-2;\n        relTol          0;\n\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    MeshPhi\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-2;\n        relTol          0;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor yes;\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors  2;\n    nCorrectors       2;\n    pRefCell          0;\n    pRefValue         0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p    0.3;\n    }\n\n    equations\n    {\n        \".*\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/mirrorMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      mirrorMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nplaneType       pointAndNormal;\n\npointAndNormalDict\n{\n    point       (0 0 0);\n    normal      (0 1 0);\n}\n\nplaneTolerance  #calc \"0.001\";\n\n// ************************************************************************* //\n",
+    "system/stirrerPower": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates the power input from the stirrer patch.\n\n\\*---------------------------------------------------------------------------*/\n\ntype            surfaceFieldValue;\nlibs            ( \"libfieldFunctionObjects.so\" );\nlog             no;\nwriteFields     no;\npatch           stirrer;\noperation       sum;\nfields          (stressUSf);\nwriteControl    outputTime;\n\n// ************************************************************************* //\n",
+    "usr_requirement": "Perform a transient incompressible stirred-reactor MRF benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application. Use the same tutorial-derived Rushton stirred tank geometry and rotating MRF cellZone as the steady MRF baseline. Use a Newtonian fluid with constant kinematic viscosity, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Use transient time discretisation with PIMPLE pressure-velocity coupling instead of steady SIMPLE. Run from t=0 to t=1 with deltaT=0.001 and write results every 100 time steps. Keep the mesh, boundary conditions, and MRF rotating-zone setup consistent with the steady MRF case. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.",
+    "_external_assets": [
+      {
+        "asset_id": "simpleRushtonMRF/stirrer4",
+        "target": "constant/geometry/stirrer4.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/stirrer6",
+        "target": "constant/geometry/stirrer6.obj"
+      },
+      {
+        "asset_id": "simpleRushtonMRF/baffles",
+        "target": "constant/geometry/baffles.obj"
+      }
+    ]
+  },
+  "MRF_stirredReactor/10": {
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    rotor\n    {\n        type            MRFnoSlip;\n    }\n\n    stator\n    {\n        type            noSlip;\n    }\n\n    front\n    {\n        type            empty;\n    }\n\n    back\n    {\n        type            empty;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    rotor\n    {\n        type            zeroGradient;\n    }\n\n    stator\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            empty;\n    }\n\n    back\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    rotor\n    {\n        type            zeroGradient;\n    }\n\n    stator\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            empty;\n    }\n\n    back\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF\n{\n    cellZone    rotor;\n\n    origin      (0 0 0);\n    axis        (0 0 1);\n\n    omega     100 [rpm];\n}\n\n// ************************************************************************* //\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          (water oil);\n\nsigma           0.05;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.oil": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.oil;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             500;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              0.0001;\n\nrho             1000;\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1.0;\n\nrHub            0.02;   // Radius of the rotor hub\nrRotorTip       0.05;   // Radius of the rotor blade tips\nrMid            0.06;   // Radius of the midpoint between rotor and stator\nrStatorTip      0.07;   // Radius of the stator blade tips\nrVessel         0.1;    // Radius of the outer vessel wall\n\nhalfDepth       0.005;  // Half-depth of the 2-D slab\n\nnCellsRootTip   12;     // Number of cells radially along the blades\nnCellsMid       4;      // Number of cells radially across the mid section (/2)\nnCellsBladeBlade 12;    // Number of cells tangentially between blades (/2)\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nvertices #codeStream\n{\n    codeInclude\n    #{\n        #include \"pointField.H\"\n        #include \"transformField.H\"\n    #};\n\n    code\n    #{\n        const pointField points0\n        ({\n            point(-$rVessel,    0, -$halfDepth),\n            point(-$rVessel,    0, -$halfDepth),\n            point(-$rStatorTip, 0, -$halfDepth),\n            point(-$rMid,       0, -$halfDepth),\n            point(-$rRotorTip,  0, -$halfDepth),\n            point(-$rHub,       0, -$halfDepth),\n            point(-$rHub,       0, -$halfDepth),\n        });\n\n        pointField points;\n        for (label i = 0; i < 8; i++)\n        {\n            points.append(transform(Rz(degToRad(i*45)), points0));\n        }\n        points.append(points + vector(0, 0, 2*$halfDepth));\n\n        os  << points;\n    #};\n};\n\nbladeBlock ($nCellsBladeBlade $nCellsRootTip 1) simpleGrading (1 1 1);\nmidBlock ($nCellsBladeBlade $nCellsMid 1) simpleGrading (1 1 1);\n\nblocks\n(\n    hex (0 8 9 2 56 64 65 58) stator $bladeBlock\n    hex (2 9 10 3 58 65 66 59) stator $midBlock\n    hex (3 10 11 4 59 66 67 60) rotor $midBlock\n    hex (4 11 12 5 60 67 68 61) rotor $bladeBlock\n\n    hex (7 14 16 9 63 70 72 65) stator $bladeBlock\n    hex (9 16 17 10 65 72 73 66) stator $midBlock\n    hex (10 17 18 11 66 73 74 67) rotor $midBlock\n    hex (11 18 20 12 67 74 76 68) rotor $bladeBlock\n\n    hex (14 22 23 16 70 78 79 72) stator $bladeBlock\n    hex (16 23 24 17 72 79 80 73) stator $midBlock\n    hex (17 24 25 18 73 80 81 74) rotor $midBlock\n    hex (18 25 26 19 74 81 82 75) rotor $bladeBlock\n\n    hex (21 28 30 23 77 84 86 79) stator $bladeBlock\n    hex (23 30 31 24 79 86 87 80) stator $midBlock\n    hex (24 31 32 25 80 87 88 81) rotor $midBlock\n    hex (25 32 34 26 81 88 90 82) rotor $bladeBlock\n\n    hex (28 36 37 30 84 92 93 86) stator $bladeBlock\n    hex (30 37 38 31 86 93 94 87) stator $midBlock\n    hex (31 38 39 32 87 94 95 88) rotor $midBlock\n    hex (32 39 40 33 88 95 96 89) rotor $bladeBlock\n\n    hex (35 42 44 37 91 98 100 93) stator $bladeBlock\n    hex (37 44 45 38 93 100 101 94) stator $midBlock\n    hex (38 45 46 39 94 101 102 95) rotor $midBlock\n    hex (39 46 48 40 95 102 104 96) rotor $bladeBlock\n\n    hex (42 50 51 44 98 106 107 100) stator $bladeBlock\n    hex (44 51 52 45 100 107 108 101) stator $midBlock\n    hex (45 52 53 46 101 108 109 102) rotor $midBlock\n    hex (46 53 54 47 102 109 110 103) rotor $bladeBlock\n\n    hex (49 0 2 51 105 56 58 107) stator $bladeBlock\n    hex (51 2 3 52 107 58 59 108) stator $midBlock\n    hex (52 3 4 53 108 59 60 109) rotor $midBlock\n    hex (53 4 6 54 109 60 62 110) rotor $bladeBlock\n);\n\narc 45 (0 0 1);\n\nedges\n(\n    arc 0 8 $arc\n    arc 7 14 $arc\n    arc 14 22 $arc\n    arc 21 28 $arc\n    arc 28 36 $arc\n    arc 35 42 $arc\n    arc 42 50 $arc\n    arc 49 0 $arc\n    arc 56 64 $arc\n    arc 63 70 $arc\n    arc 70 78 $arc\n    arc 77 84 $arc\n    arc 84 92 $arc\n    arc 91 98 $arc\n    arc 98 106 $arc\n    arc 105 56 $arc\n\n    arc 2 9 $arc\n    arc 9 16 $arc\n    arc 16 23 $arc\n    arc 23 30 $arc\n    arc 30 37 $arc\n    arc 37 44 $arc\n    arc 44 51 $arc\n    arc 51 2 $arc\n    arc 58 65 $arc\n    arc 65 72 $arc\n    arc 72 79 $arc\n    arc 79 86 $arc\n    arc 86 93 $arc\n    arc 93 100 $arc\n    arc 100 107 $arc\n    arc 107 58 $arc\n\n    arc 3 10 $arc\n    arc 10 17 $arc\n    arc 17 24 $arc\n    arc 24 31 $arc\n    arc 31 38 $arc\n    arc 38 45 $arc\n    arc 45 52 $arc\n    arc 52 3 $arc\n    arc 59 66 $arc\n    arc 66 73 $arc\n    arc 73 80 $arc\n    arc 80 87 $arc\n    arc 87 94 $arc\n    arc 94 101 $arc\n    arc 101 108 $arc\n    arc 108 59 $arc\n\n    arc 4 11 $arc\n    arc 11 18 $arc\n    arc 18 25 $arc\n    arc 25 32 $arc\n    arc 32 39 $arc\n    arc 39 46 $arc\n    arc 46 53 $arc\n    arc 53 4 $arc\n    arc 60 67 $arc\n    arc 67 74 $arc\n    arc 74 81 $arc\n    arc 81 88 $arc\n    arc 88 95 $arc\n    arc 95 102 $arc\n    arc 102 109 $arc\n    arc 109 60 $arc\n\n    arc 5 12 $arc\n    arc 12 20 $arc\n    arc 19 26 $arc\n    arc 26 34 $arc\n    arc 33 40 $arc\n    arc 40 48 $arc\n    arc 47 54 $arc\n    arc 54 6 $arc\n    arc 61 68 $arc\n    arc 68 76 $arc\n    arc 75 82 $arc\n    arc 82 90 $arc\n    arc 89 96 $arc\n    arc 96 104 $arc\n    arc 103 110 $arc\n    arc 110 62 $arc\n);\n\ndefaultPatch\n{\n    name walls;\n    type wall;\n}\n\nboundary\n(\n    rotor\n    {\n        type wall;\n        faces\n        (\n            (5 61 68 12)\n            (12 68 76 20)\n            (19 75 82 26)\n            (26 82 90 34)\n            (33 89 96 40)\n            (40 96 104 48)\n            (47 103 110 54)\n            (54 110 62 6)\n\n            (4 60 62 6)\n            (18 74 76 20)\n            (32 88 90 34)\n            (46 102 104 48)\n            (4 5 61 60)\n            (18 19 75 74)\n            (32 33 89 88)\n            (46 47 103 102)\n        );\n    }\n    stator\n    {\n        type wall;\n        faces\n        (\n            (0 8 64 56)\n            (7 14 70 63)\n            (14 22 78 70)\n            (21 28 84 77)\n            (28 36 92 84)\n            (35 42 98 91)\n            (42 50 106 98)\n            (49 0 56 105)\n\n            (8 64 65 9)\n            (22 78 79 23)\n            (36 92 93 37)\n            (50 106 107 51)\n            (7 9 65 63)\n            (21 23 79 77)\n            (35 37 93 91)\n            (49 51 107 105)\n        );\n    }\n    front\n    {\n        type empty;\n        faces\n        (\n            (56 58 65 64)\n            (63 65 72 70)\n            (70 72 79 78)\n            (77 79 86 84)\n            (84 86 93 92)\n            (91 93 100 98)\n            (98 100 107 106)\n            (105 107 58 56)\n\n            (58 59 66 65)\n            (65 66 73 72)\n            (72 73 80 79)\n            (79 80 87 86)\n            (86 87 94 93)\n            (93 94 101 100)\n            (100 101 108 107)\n            (107 108 59 58)\n\n            (59 60 67 66)\n            (66 67 74 73)\n            (73 74 81 80)\n            (80 81 88 87)\n            (87 88 95 94)\n            (94 95 102 101)\n            (101 102 109 108)\n            (108 109 60 59)\n\n            (60 61 68 67)\n            (67 68 76 74)\n            (74 75 82 81)\n            (81 82 90 88)\n            (88 89 96 95)\n            (95 96 104 102)\n            (102 103 110 109)\n            (109 110 62 60)\n        );\n    }\n    back\n    {\n        type empty;\n        faces\n        (\n            (0 2 9 8)\n            (7 9 16 14)\n            (14 16 23 22)\n            (21 23 30 28)\n            (28 30 37 36)\n            (35 37 44 42)\n            (42 44 51 50)\n            (49 51 2 0)\n\n            (2 3 10 9)\n            (9 10 17 16)\n            (16 17 24 23)\n            (23 24 31 30)\n            (30 31 38 37)\n            (37 38 45 44)\n            (44 45 52 51)\n            (51 52 3 2)\n\n            (3 4 11 10)\n            (10 11 18 17)\n            (17 18 25 24)\n            (24 25 32 31)\n            (31 32 39 38)\n            (38 39 46 45)\n            (45 46 53 52)\n            (52 53 4 3)\n\n            (4 5 12 11)\n            (11 12 20 18)\n            (18 19 26 25)\n            (25 26 34 32)\n            (32 33 40 39)\n            (39 40 48 46)\n            (46 47 54 53)\n            (53 54 6 4)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          incompressibleVoF;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         5;\ndeltaT          1e-3;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.01;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  yes;\n\nmaxCo           0.5;\nmaxAlphaCo      0.5;\n\nmaxDeltaT       1;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    div(rhoPhi,U)  Gauss linear;\n    div(phi,alpha)  Gauss interfaceCompression vanLeer 1;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    alpha.water\n    {\n        nCorrectors     1;\n        nSubCycles      polynomial (0 2);\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-10;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-07;\n        relTol          0.05;\n    }\n\n    p_rghFinal\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-07;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-06;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor no;\n    nCorrectors     3;\n    nNonOrthogonalCorrectors 0;\n\n    pRefCell        0;\n    pRefValue       0;\n}\n\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "FoamFile\n{ format ascii; class dictionary; object setFieldsDict; }\ndefaultFieldValues (volScalarFieldValue alpha.water 0);\nregions\n(\n    boxToCell\n    {\n        box (-0.1 -0.1 -1) (0.1 0.1 0.0025);\n        fieldValues (volScalarFieldValue alpha.water 1);\n    }\n);\n",
+    "usr_requirement": "Perform a two-phase liquid-liquid stirred-reactor MRF benchmark using water and oil with incompressibleVoF. Initialise a finite oil layer over a water region using OpenFOAM-13 setFields syntax, use zero gravity and retain p_rgh, interface compression, adaptive time stepping, and a 100 rpm MRF rotor. This is the water/oil variant, distinct from the single-phase laminar, turbulence, baffle, rheology, NCC, and transient variants. Use an eight-sector rotor-stator vessel with outer radius 0.10 m, rotor-tip radius 0.05 m, stator-tip radius 0.07 m and a 0.01 m quasi-2D thickness. Water has density 1000 kg/m3 and kinematic viscosity 1e-4 m2/s; oil has density 500 kg/m3 and the same viscosity; surface tension is 0.05 N/m and gravity is zero. Initially the lower portion up to z=0.0025 m is water and the rest is oil."
+  },
+  "ERCOFTA_pump/1": {
+    "usr_requirement": "Perform a steady incompressible ERCOFTA pump reference case using OpenFOAM-13 with foamRun -solver incompressibleFluid, using the tutorial-style MRF rotating-machine setup with a rotor cellZone, inlet/outlet boundaries, and wall patches for the blade and shroud surfaces. Keep the design-speed rotation rate and the baseline RANS closure fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use an incompressible liquid with kinematic viscosity 1e-6 m2/s, a volumetric inlet flow of 0.03473 m3/s and zero-gauge outlet pressure. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver incompressibleFluid\n\n#------------------------------------------------------------------------------\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        volumetricFlowRate 0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O  operation     | Website:  https://openfoam.org\n    \\\\  /    A  nd           | Version:  13\n     \\\\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O  operation     | Website:  https://openfoam.org\n    \\\\  /    A  nd           | Version:  13\n     \\\\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    k\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    kFinal\n    {\n        $k;\n        relTol          0;\n    }\n\n    omega\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    omegaFinal\n    {\n        $omega;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O  peration     | Website:  https://openfoam.org\n    \\\\  /    A  nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O  peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              1e-06;\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/2": {
+    "usr_requirement": "Perform a steady compressible ERCOFTA pump reference case using OpenFOAM-13 with foamRun -solver fluid, keeping the tutorial-style rotating-region setup, the rotor cellZone, inlet/outlet boundaries, and the baseline RANS closure fixed. Retain the compressible thermophysical settings and the design-speed rotation rate. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/3": {
+    "usr_requirement": "Perform a steady ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-region setup as the baseline but changing only the rotating speed away from the design RPM. Keep the rotor cellZone, boundary layout, turbulence model, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -25 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -25;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/4": {
+    "usr_requirement": "Perform the steady compressible ERCOFTA rotating-region surrogate with foamRun -solver fluid and change only the OUTLET fixed pressure from the 101325 Pa baseline to 120000 Pa. Keep the rotor cellZone, omega=-20, kOmegaSST, thermophysical model, mesh, boundaries, steady SIMPLE settings, endTime=0.001, deltaT=5e-7, and writeInterval=1 fixed. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 120000 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 120000;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 120000;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/5": {
+    "usr_requirement": "Perform a transient compressible ERCOFTA rotating-region surrogate using foamRun -solver fluid with the same perfect-gas thermophysical model, inlet/outlet conditions, U field, omega=-20, mesh, and rotor cellZone as the compressible baseline. Change only the temporal/turbulence treatment to Euler + PIMPLE with LES kOmegaSSTDES; use endTime=0.001, deltaT=1e-6, and writeInterval=1. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          1e-6;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  LES;\n\nLES\n{\n    model           kOmegaSSTDES;\n\n    delta           cubeRootVol;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff 1;\n    }\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/6": {
+    "usr_requirement": "Perform a steady ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-region setup as the baseline but switching only the turbulence model to kEpsilon. Keep the rotor cellZone, rotating speed, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,epsilon) bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|epsilon|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega|epsilon)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega|epsilon)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model kEpsilon;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform 0.0002025;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            epsilonWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            epsilonWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            epsilonWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            epsilonWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/7": {
+    "usr_requirement": "Perform a steady compressible ERCOFTA rotating-region surrogate with foamRun -solver fluid as a rotor-zone-extent sensitivity case. Extend only the boxToCell rotor region from the baseline x=0..0.3 to x=0..0.45 while retaining omega=-20, RAS kOmegaSST, thermophysical fields, mesh, boundary conditions, steady SIMPLE settings, endTime=0.001, deltaT=5e-7, and writeInterval=1. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.45 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/8": {
+    "usr_requirement": "Perform a steady compressible ERCOFTA rotating-region surrogate using foamRun -solver fluid with omega=-15, retaining the baseline kOmegaSST, perfect-gas thermophysical model, rotor zone, mesh, boundaries, steady SIMPLE controls, and post-processing. This is the low-speed companion to omega=-20 baseline and omega=-25 variant. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -15 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -15;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/9": {
+    "usr_requirement": "Perform a transient ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-machinery setup as the baseline but using the legacy rhoPimpleFoam-style transient PIMPLE coupling. Keep the rotor cellZone, rotating speed, turbulence model, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\n#------------------------------------------------------------------------------\nrunApplication foamRun -solver fluid\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (24 8 16) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "ERCOFTA_pump/10": {
+    "usr_requirement": "Perform a steady compressible ERCOFTA rotating-machine surrogate using foamRun -solver fluid. Change only the uniform rectangular surrogate mesh from 24x8x16 to 48x16x32; retain omega=-20, RAS kOmegaSST, thermophysical fields, boundaries, steady discretisation, and run controls. This is the fine-mesh resolution variant, not a claim of supplied double-row blade geometry. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication topoSet\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            compressible::alphatWallFunction;\n        Prt             0.85;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0.01;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_ROT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    BLADE_STAT\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n    HUB_SHROUD\n    {\n        type            kqRWallFunction;\n        value           uniform 0.01;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    INLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    OUTLET\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n    STATOR\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_ROT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    BLADE_STAT\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n    HUB_SHROUD\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform 10;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_ROT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    BLADE_STAT\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n    HUB_SHROUD\n    {\n        type            omegaWallFunction;\n        value           uniform 10;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 101325;\n\nboundaryField\n{\n    INLET\n    {\n        type            zeroGradient;\n    }\n    OUTLET\n    {\n        type            fixedValue;\n        value           uniform 101325;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    INLET\n    {\n        type            fixedValue;\n        value           uniform 300;\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n    }\n    STATOR\n    {\n        type            zeroGradient;\n    }\n    BLADE_ROT\n    {\n        type            zeroGradient;\n    }\n    BLADE_STAT\n    {\n        type            zeroGradient;\n    }\n    HUB_SHROUD\n    {\n        type            zeroGradient;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    INLET\n    {\n        type            flowRateInletVelocity;\n        massFlowRate    0.03473;\n        value           uniform (0 0 0);\n    }\n    OUTLET\n    {\n        type            zeroGradient;\n        value           uniform (0 0 0);\n    }\n    STATOR\n    {\n        type            noSlip;\n    }\n    BLADE_ROT\n    {\n        type            MRFnoSlip;\n        value           uniform (0 0 0);\n    }\n    BLADE_STAT\n    {\n        type            fixedValue;\n        value           uniform (0 0 0);\n    }\n    HUB_SHROUD\n    {\n        type            noSlip;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nMRF1\n{\n    cellZone    rotor;\n    active      yes;\n\n    nonRotatingPatches (INLET OUTLET);\n\n    origin    (0 0 0);\n    axis      (0 0 1);\n    omega     -20;\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.001;\n\ndeltaT          5e-7;\n\nwriteControl    timeStep;\n\nwriteInterval   1;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression on;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable yes;\n\nadjustTimeStep  no;\nmaxCo           0.5;\n\nfunctions\n{\n};\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n    grad(U)         cellLimited Gauss linear 1;\n    grad(k)         cellLimited Gauss linear 1;\n    grad(omega)     cellLimited Gauss linear 1;\n}\n\ndivSchemes\n{\n    default         none;\n    div(phi,U)      bounded Gauss upwind;\n    div(phi,k)      bounded Gauss upwind;\n    div(phi,omega)  bounded Gauss upwind;\n    div(phi,K)      bounded Gauss upwind;\n    div(phi,T)      bounded Gauss upwind;\n    div(phi,h)      bounded Gauss upwind;\n    div(phi,e)      bounded Gauss upwind;\n    div(phi,Ekp)    bounded Gauss upwind;\n    div(phi,(p|rho)) bounded Gauss upwind;\n    div((phi|interpolate(rho)),p) Gauss upwind;\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method          meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(rho|U|h|e|T|k|omega|alphat)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    nNonOrthogonalCorrectors 0;\n    consistent      yes;\n\n    pRefCell        0;\n    pRefValue       0;\n\n    residualControl\n    {\n        p               1e-5;\n        U               1e-5;\n        \"(T|h|e|k|omega)\" 1e-5;\n    }\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.3;\n        \"(T|h|e|k|omega)\" 0.3;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  RAS;\n\nRAS\n{\n    model           kOmegaSST;\n\n    turbulence      on;\n\n    printCoeffs     on;\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (0 0 0)\n    (0.6 0 0)\n    (0.6 0.25 0)\n    (0 0.25 0)\n    (0 0 0.2)\n    (0.6 0 0.2)\n    (0.6 0.25 0.2)\n    (0 0.25 0.2)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (48 16 32) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    INLET\n    {\n        type patch;\n        faces ((0 4 7 3));\n    }\n\n    OUTLET\n    {\n        type patch;\n        faces ((1 2 6 5));\n    }\n\n    STATOR\n    {\n        type wall;\n        faces ((0 1 5 4));\n    }\n\n    BLADE_ROT\n    {\n        type wall;\n        faces ((3 7 6 2));\n    }\n\n    BLADE_STAT\n    {\n        type wall;\n        faces ((0 3 2 1));\n    }\n\n    HUB_SHROUD\n    {\n        type wall;\n        faces ((4 5 6 7));\n    }\n);\n\nmergePatchPairs\n(\n);\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    rotorCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (0 0 0) (0.3 0.25 0.2);\n    }\n\n    {\n        name    rotor;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rotorCells;\n    }\n);\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture\n{\n    specie\n    {\n        nMoles      1;\n        molWeight   28.9643899421023;\n    }\n    thermodynamics\n    {\n        Cp          1004.70300000000;\n        Hf          0;\n\tTref        0;\n    }\n    transport\n    {\n        mu           1.8e-5;\n        Pr           0.72;\n    }\n}\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F  ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O  peration     | Website:  https://openfoam.org\n    \\  /    A  nd           | Version:  13\n     \\/     M  anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nlimitp\n{\n    type       limitPressure;\n\n    min        0.8e5;\n    max        1.2e5;\n}\n\n\nboundK\n{\n    type       bound;\n\n    field      k;\n\n    min        1e-12;\n}\n\nboundOmega\n{\n    type       bound;\n\n    field      omega;\n\n    min        1e-12;\n}\n\n// ************************************************************************* //\n"
+  },
+  "compressibleBubbleCollapse/1": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. This is the baseline single-bubble case with a circular gas bubble of radius 50um centered in the domain at 5MPa ambient pressure, using the same 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport as the shared baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "compressibleBubbleCollapse/2": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble radius, using two radius subcases of 100um and 200um, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, bubble center, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the 50um baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n",
+    "reference_subcases": [
+      {
+        "id": "radius100um",
+        "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble radius, using a 100um bubble while keeping the 2D 10mm-high domain, 5MPa ambient pressure, bubble center, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the 50um baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+        "overrides": {
+          "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*      =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.0001;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+          "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+          "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n"
+        }
+      },
+      {
+        "id": "radius200um",
+        "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble radius, using a 200um bubble while keeping the 2D 10mm-high domain, 5MPa ambient pressure, bubble center, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the 50um baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+        "overrides": {
+          "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*      =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.0002;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+          "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+          "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n"
+        }
+      }
+    ]
+  },
+  "compressibleBubbleCollapse/3": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the ambient pressure, using a weak-collapse branch at 2MPa and a strong-collapse branch at 10MPa, while keeping the 50um single bubble, centered placement, 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n",
+    "reference_subcases": [
+      {
+        "id": "ambient2MPa",
+        "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the ambient pressure, using a weak-collapse branch at 2MPa while keeping the 50um single bubble, centered placement, 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+        "overrides": {
+          "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 2000000\n    volScalarFieldValue p 2000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+          "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 2000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 2000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+          "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 2000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 2000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n"
+        }
+      },
+      {
+        "id": "ambient10MPa",
+        "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the ambient pressure, using a strong-collapse branch at 10MPa while keeping the 50um single bubble, centered placement, 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+        "overrides": {
+          "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 10000000\n    volScalarFieldValue p 10000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+          "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 10000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 10000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+          "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 10000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 10000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n"
+        }
+      }
+    ]
+  },
+  "compressibleBubbleCollapse/4": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the bubble-center distance from the solid wall, placing the 50um bubble in a near-wall configuration, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Place the bubble centre 0.20 mm above the bottom wall.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.0002);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "compressibleBubbleCollapse/5": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble shape, replacing the circular 50um baseline bubble with a stepped/asymmetric axis-aligned rectangular initial contour represented by two boxToCell selections at the same center location, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport unchanged. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Form the asymmetric bubble from two overlapping rectangles: one spanning radial coordinate -53.79 to 26.21 um and height 4.9625 to 5.0375 mm, and the second spanning 26.21 to 63.21 um and height 4.975 to 5.025 mm.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    boxToCell\n    {\n        box (-5.379e-5 -2e-5 0.0049625) (2.621e-5 2e-5 0.0050375);\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n    boxToCell\n    {\n        box (2.621e-5 -2e-5 0.004975) (6.321e-5 2e-5 0.005025);\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "compressibleBubbleCollapse/6": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the gas-liquid density ratio, using a lighter-gas branch by lowering the air density while keeping the liquid model, the 50um bubble geometry, the 2D 10mm-high domain, the 5MPa ambient pressure, and the interfaceCompression + vanLeer VOF transport fixed to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 14.48 and Cp=2009.406 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       14.48;\n    }\n    thermodynamics\n    {\n        Cp              2009.406;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "compressibleBubbleCollapse/7": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the mesh strategy by enabling AMR around the gas-liquid interface with dynamicRefineFvMesh, while keeping the 50um single bubble, 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n",
+    "constant/dynamicMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      dynamicMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntopoChanger\n{\n    type            refiner;\n\n    libs            (\"libfvMeshTopoChangers.so\");\n\n    mover           none;\n\n    refineInterval  1;\n\n    field           alpha.water;\n\n    lowerRefineLevel 0.001;\n    upperRefineLevel 0.999;\n\n    nBufferLayers   1;\n\n    maxRefinement   2;\n\n    maxCells        200000;\n\n    correctFluxes\n    (\n        (phi none)\n        (nHatf none)\n        (rhoPhi none)\n        (alphaPhi.water none)\n        (alphaPhi.air none)\n        (alphaRhoPhi.water none)\n        (alphaRhoPhi.air none)\n        (ghf none)\n    );\n\n    dumpLevel       true;\n}\n\n// ************************************************************************* //\n"
+  },
+  "compressibleBubbleCollapse/8": {
+    "usr_requirement": "Perform the fixed uniform fine-mesh compressible bubble-collapse baseline using foamRun -solver compressibleVoF. Keep the 50 um bubble, 5 MPa pressure, thermophysical model, interface scheme, and controls fixed while refining the uniform base mesh from 200x1x200 to 400x1x400. This is the fixed-grid resolution counterpart to the adaptive-AMR variant. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 400;\nny 1;\nnz 400;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "compressibleBubbleCollapse/9": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Change only the solver family and compressibility treatment for an incompressible VOF comparison, while keeping the same 50um bubble placement, 2D 10mm-high domain, water/air interface geometry, and as much of the baseline setup as the solver allows. This branch is the incompressible interFoam-style reference against the compressible bubble-collapse baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For this incompressible comparison use water rho=998 kg/m3 and nu=3.653e-7 m2/s, air rho=1.2 kg/m3 and nu=1.533e-5 m2/s.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"incompressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver $solver\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases          ( water air );\n\nsigma           sigma [ 1 0 -2 0 0 0 0 ] 0;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleVoF;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,U)                                 Gauss upwind;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    U\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    UFinal\n    {\n        $U;\n        relTol          0;\n    }\n\n    pcorr\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-6;\n        relTol          0;\n    }\n\n    pcorrFinal\n    {\n        $pcorr;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 1.533e-5;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 1.2;\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  Newtonian;\n\nnu              nu [ 0 2 -1 0 0 0 0 ] 3.653e-7;\n\nrho             rho [ 1 -3 0 0 0 0 0 ] 998;\n\n// ************************************************************************* //\n"
+  },
+  "compressibleBubbleCollapse/10": {
+    "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the number of bubbles by introducing a second identical 50um bubble so the two bubbles interact, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the single-bubble baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Place the second 50 um bubble 0.15 mm from the first in the radial direction.",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nsolver=\"compressibleVoF\"\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver $solver\nrunApplication reconstructPar -newTimes\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    WALL\n    {\n        type            noSlip;\n    }\n    TOP\n    {\n        type            zeroGradient;\n    }\n    SIDE\n    {\n        type            zeroGradient;\n    }\n    front\n    {\n        type            wedge;\n    }\n    back\n    {\n        type            wedge;\n    }\n    axis\n    {\n        type            empty;\n    }\n}\n",
+    "constant/g": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       uniformDimensionedVectorField;\n    location    \"constant\";\n    object      g;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -2 0 0 0 0];\nvalue           (0 0 0);\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/phaseProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      phaseProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nphases (water air);\n\npMin        3350;\n\nsigma\n{\n    type    constant;\n    sigma   0.0;\n}\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nxx 0.0099904822;  // radial; r*cos(2.5deg) = r*0.99904822\nyp 0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nym -0.00043619387;  // polar;  r*sin(2.5deg) = r*0.043619387\nzz 0.01;\n\n// number of points\nnx 200;\nny 1;\nnz 200;\n\nvertices\n(\n    (0   0    0)\n    ($xx $ym  0)\n    ($xx $yp  0)\n    (0   0    $zz)\n    ($xx $ym  $zz)\n    ($xx $yp  $zz)\n);\n\nblocks\n(\n    hex (0 1 2 0 3 4 5 3) ($nx $ny $nz) simpleGrading (1 1 1)\n);\n\n\nedges\n(\n);\n\nboundary\n(\n    WALL\n    {\n        type patch;\n        faces\n        (\n            (0 1 2 0)\n        );\n    }\n    TOP\n    {\n        type patch;\n        faces\n        (\n            (3 4 5 3)\n        );\n    }\n    SIDE\n    {\n        type wall;\n        faces\n        (\n            (1 2 5 4)\n        );\n    }\n    front\n    {\n        type wedge;\n        faces\n        (\n            (0 1 4 3)\n        );\n    }\n    back\n    {\n        type wedge;\n        faces\n        (\n            (2 0 3 5)\n        );\n    }\n    axis\n    {\n        type empty;\n        faces\n        (\n            (0 3 3 0)\n        );\n    }\n);\n\nmergePatchPairs\n(\n);\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          compressibleVoF;\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1e-7;\n\ndeltaT          1e-10;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   1e-8;\n\npurgeWrite      20;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   10;\n\nrunTimeModifiable yes;\nadjustTimeStep  yes;\nmaxCo           0.3;\nmaxAlphaCo      1;\nmaxDeltaT       2e-9;\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 3;\n\nmethod          scotch;\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default                                    none;\n    div(phi,alpha)                             Gauss interfaceCompression vanLeer 1;\n    div(phirb,alpha)                           Gauss interfaceCompression vanLeer 1;\n    div(rhoPhi,U)                              Gauss upwind;\n    div(rhoPhi,T)                              Gauss upwind;\n    div(phi,k)                                 Gauss upwind;\n    div(phi,omega)                             Gauss upwind;\n    div(rhoPhi,K)                      Gauss upwind;\n    div(phi,p)                                 Gauss upwind;\n    div(phid,p)                                Gauss upwind;\n    div(rhoPhi,p)                              Gauss upwind;\n    div(rhoPhi,e)                              Gauss upwind;\n    div(rhoPhi,h)                              Gauss upwind;\n    div(alphaRhoPhi,e)                         Gauss upwind;\n    div(alphaRhoPhi.air,e.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,e.water)             Gauss upwind;\n    div(alphaRhoPhi,h)                         Gauss upwind;\n    div(alphaRhoPhi.air,h.air)                 Gauss upwind;\n    div(alphaRhoPhi.water,h.water)             Gauss upwind;\n    div(alphaRhoPhi,T)                         Gauss upwind;\n    div(alphaRhoPhi.air,T)                     Gauss upwind;\n    div(alphaRhoPhi.water,T)                   Gauss upwind;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"alpha.*\"\n    {\n        nAlphaCorr      1;\n        nAlphaSubCycles 2;\n\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-8;\n        relTol          0;\n    }\n\n    p_rgh\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    p_rghFinal\n    {\n        $p_rgh;\n        relTol          0;\n    }\n\n    p\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0.01;\n    }\n\n    \"pcorr.*\"\n    {\n        solver          PCG;\n        preconditioner  DIC;\n        tolerance       1e-7;\n        relTol          0;\n        maxIter         100;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-8;\n        relTol          0.1;\n    }\n\n    \"(U|T|e.*|h.*|rho.*)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    momentumPredictor   yes;\n    nOuterCorrectors    1;\n    nCorrectors         2;\n    nNonOrthogonalCorrectors 0;\n}\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volScalarFieldValue alpha.water 1\n    volScalarFieldValue p_rgh 5000000\n    volScalarFieldValue p 5000000\n    volScalarFieldValue T 300\n);\n\nregions\n(\n    sphereToCell\n    {\n        centre (0 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n    sphereToCell\n    {\n        centre (0.00015 0 0.005);\n        radius 0.00005;\n        fieldValues\n        (\n            volScalarFieldValue alpha.water 0\n            volScalarFieldValue p_rgh 3550\n            volScalarFieldValue p 3550\n            volScalarFieldValue T 300\n        );\n    }\n);\n",
+    "0/alpha.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      alpha.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p_rgh": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p_rgh;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 5000000;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            fixedValue;\n        value           uniform 5000000;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 300;\n\nboundaryField\n{\n    WALL\n    {\n        type            zeroGradient;\n    }\n\n    TOP\n    {\n        type            zeroGradient;\n    }\n\n    SIDE\n    {\n        type            zeroGradient;\n    }\n\n    front\n    {\n        type            wedge;\n    }\n\n    back\n    {\n        type            wedge;\n    }\n\n    axis\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties.air": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.air;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\n\nmixture\n{\n    specie\n    {\n        molWeight       28.96;\n    }\n    thermodynamics\n    {\n        Cp              1004.5;\n        Hf              0;\n    }\n    transport\n    {\n        mu              1.84e-05;\n        Pr              0.7;\n    }\n}\n",
+    "constant/physicalProperties.water": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties.water;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            heRhoThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          eConst;\n    equationOfState perfectFluid;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight   18;\n    }\n    equationOfState\n    {\n        R           100000;\n        rho0        998;\n    }\n    thermodynamics\n    {\n        Cv          4195;\n        Hf          0;\n    }\n    transport\n    {\n        mu          3.645e-4;\n        Pr          2.289;\n    }\n}\n"
+  },
+  "aerofoilNACA0012/1": {
+    "usr_requirement": "Perform a low-subsonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.15 at zero angle of attack; set speed=52 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           52;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/2": {
+    "usr_requirement": "Perform a subsonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at zero angle of attack; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/3": {
+    "usr_requirement": "Perform a transonic-onset NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.7 at zero angle of attack; set speed=242 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           242;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/4": {
+    "usr_requirement": "Perform a transonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.8 at zero angle of attack; set speed=277 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           277;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/5": {
+    "usr_requirement": "Perform a negative-five-degree NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=-5 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=-5 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   -5; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/6": {
+    "usr_requirement": "Perform a five-degree angle-of-attack NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=5 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=5 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=1000; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   5; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1000;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-08;\n        relTol          0.01;\n    }\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-06;\n        U               1e-05;\n        \"(k|omega|epsilon|nuTilda|h)\" 1e-05;\n    }\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors 4;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.2;\n        rho             0.01;\n    }\n    equations\n    {\n        U               0.3;\n        h               0.3;\n        \"(k|omega|epsilon|nuTilda)\" 0.7;\n        k               0.3;\n        omega           0.3;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/7": {
+    "usr_requirement": "Perform a ten-degree angle-of-attack NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=10 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=10 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=1500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   10; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision  10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n        tolerance       1e-08;\n        relTol          0.01;\n    }\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-06;\n        U               1e-05;\n        \"(k|omega|epsilon|nuTilda|h)\" 1e-05;\n    }\n    nNonOrthogonalCorrectors 0;\n    nOuterCorrectors 4;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.2;\n        rho             0.01;\n    }\n    equations\n    {\n        U               0.3;\n        h               0.3;\n        \"(k|omega|epsilon|nuTilda)\" 0.7;\n        k               0.3;\n        omega           0.3;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/8": {
+    "usr_requirement": "Perform a NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid and a snappyHexMesh multi-level refinement strategy. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at AoA=0 degrees; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model. Generate a background mesh and apply snappyHexMesh refinement around the aerofoil surface, near-field region, and downstream wake while preserving extruded front/back constraint patches for a quasi-2D aerofoil calculation. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, blockMesh/snappyHexMesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication snappyHexMesh -overwrite\nrunApplication checkMesh\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   0; // degs\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $Uinlet;\n    }\n\n    outlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    outlet\n    {\n        type            fixedValue;\n        value           uniform $pOut;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n        value           uniform $pOut;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $Tinlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           uniform $Tinlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           uniform $Tinlet;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    outlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -4;\nxMax    5;\nyMin   -0.6;\nyMax    0.6;\nzMin   -2;\nzMax    2;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (90 1 40) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces ((0 4 7 3));\n    }\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces ((1 2 6 5));\n    }\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    back\n    {\n        type symmetryPlane;\n        faces ((0 3 2 1));\n    }\n    front\n    {\n        type symmetryPlane;\n        faces ((4 5 6 7));\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    aerofoil\n    {\n        type triSurface;\n        file \"NACA0012.obj\";\n    }\n\n    nearfield\n    {\n        type box;\n        min (-0.5 -0.55 -0.5);\n        max ( 1.5  0.55  0.5);\n    }\n\n    wake\n    {\n        type box;\n        min ( 1.0 -0.55 -0.6);\n        max ( 4.5  0.55  0.6);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        aerofoil\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        nearfield\n        {\n            mode inside;\n            level 1;\n        }\n\n        wake\n        {\n            mode inside;\n            level 1;\n        }\n    }\n\n    insidePoint (0.5 0 1);\n    nCellsBetweenLevels 3;\n}\n\nsnapControls {}\n\naddLayersControls {}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          1e-3;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    outlet\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    back\n    {\n        type            symmetryPlane;\n    }\n\n    front\n    {\n        type            symmetryPlane;\n    }\n\n    aerofoil\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/9": {
+    "usr_requirement": "Perform a transient compressible NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid, corresponding to the legacy rhoPimpleFoam-style workflow. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at AoA=0 degrees; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Use transient time discretisation and PIMPLE pressure-velocity coupling suitable for the rhoPimpleFoam replacement path. Run from t=0 to t=0.15; deltaT=2e-5; write results every 0.001 simulation-time units using writeControl=adjustableRunTime. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    outlet\n    {\n        type            waveTransmissive;\n        field           p;\n        gamma           1.4;\n        fieldInf        $pOut;\n        lInf            5;\n        value           uniform $pOut;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n    turbulence          on;\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         0.15;\n\ndeltaT          2e-5;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.001;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n//************************************************************************** //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default             none;\n\n    div(phi,U)          Gauss linearUpwind limited;\n\n    turbulence          Gauss linearUpwind limited;\n    energy              Gauss linearUpwind limited;\n\n    div(phi,k)          $turbulence;\n    div(phi,omega)      $turbulence;\n\n    div(phi,e)          $energy;\n    div(phi,K)          $energy;\n    div(phi,Ekp)        $energy;\n    div(phi,(p|rho))    $energy;\n\n    div((phi|interpolate(rho)),p) Gauss upwind;\n\n    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.01;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol          0;\n    }\n\n    \"(rho|U|k|omega|e)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(rho|U|k|omega|e)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|e)\"   1e-4;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nPIMPLE\n{\n    nCorrectors              2;\n    nNonOrthogonalCorrectors 1;\n    nOuterCorrectors         1;\n}\n\nrelaxationFactors\n{\n    equations\n    {\n        \".*\"     1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMin -4;\n    xMax  4;\n    zMin -2;\n    zMax  2;\n\n    // Number of cells\n    zCells  80; // aerofoil to far field\n    xUCells 30; // upstream\n    xMCells 30; // middle\n    xDCells 40; // downstream\n\n    // Mesh grading\n    zGrading    40;  // aerofoil to far field\n    xUGrading   5;   // towards centre upstream\n    leadGrading 0.2; // towards leading edge\n    xDGrading   10;  // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n    xLower  0.3;\n    zLower -0.06;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     0.1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.01;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      10;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "aerofoilNACA0012/10": {
+    "usr_requirement": "Perform a steady compressible NACA0012 aerofoil turbulence variant using foamRun -solver fluid with the 2D structured/snappy geometry, SpalartAllmaras RAS, steady SIMPLE controls, and the same Mach 0.5, AoA=0, mesh, thermophysical fields, and forceCoeffs workflow as the baseline. This is the economical 2D SA-RANS alternative to the baseline kOmegaSST case; it does not claim DDES. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.",
+    "_external_assets": [
+      {
+        "asset_id": "naca0012/NACA0012",
+        "target": "constant/geometry/NACA0012.obj.gz"
+      }
+    ],
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication transformPoints \"scale=(1 0 1)\"\nrunApplication extrudeMesh\n\nrunApplication foamRun -solver fluid\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nspeed           173;\nangleOfAttack   0; // degs\n\nangle           #calc \"-degToRad($angleOfAttack)\";\n\n#calcInclude    \"transform.H\"\nliftDir         #calc \"transform(Ry($angle), vector(0, 0, 1))\";\ndragDir         #calc \"transform(Ry($angle), vector(1, 0, 0))\";\n\nUinlet          #calc \"$speed*$<vector>dragDir\";\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform $Uinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform $Uinlet;\n        value           uniform $Uinlet;\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\npOut            1e5;\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform $pOut;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform $pOut;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nTinlet          298;\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform $Tinlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $Tinlet;\n        value           $inletValue;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/alphat": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      alphat;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            compressible::alphatWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      mut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "FoamFile\n{\n    format ascii;\n    class dictionary;\n    object momentumTransport;\n}\nsimulationType RAS;\nRAS\n{\n    model               SpalartAllmaras;\n    turbulence          on;\n    printCoeffs         on;\n}\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleEnthalpy;\n}\n\nmixture // air at room temperature (293 K)\n{\n    specie\n    {\n        molWeight   28.9;\n    }\n\n    thermodynamics\n    {\n        Cp          1005;\n        hf          0;\n    }\n\n    transport\n    {\n        mu          1.82e-05;\n        Pr          0.71;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          fluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         500;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     ascii;\n\nwritePrecision   10;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsCompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     |\n    \\\\  /    A nd           | Web:      www.OpenFOAM.org\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is compressible (pressure is\n    in units M/(LT^2), e.g. Pa).\n\n\\*---------------------------------------------------------------------------*/\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (aerofoil);\n\nmagUInf     $speed;\nlRef        1;\nAref        1; // span\nrhoInf      1.2;\n\nCofR        (0.2 0 0);\npitchAxis   (0 1 0);\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffs.cfg\"\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc MachNo\n#includeFunc residuals\n#includeFunc forceCoeffsCompressible\n\n// ************************************************************************* //\n",
+    "system/fvConstraints": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvConstraints;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeConstraint limitPressure(minFactor=0.1, maxFactor=2)\n#includeConstraint limitTemperature(min=101, max=1000)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n    grad(epsilon)   $limited;\n    grad(nuTilda)   $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    energy          bounded Gauss linearUpwind limited;\n    div(phi,h)      $energy;\n    div(phi,K)      $energy;\n\n    turbulence      bounded Gauss upwind;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div(((rho*nuEff)*dev2(T(grad(U)))))    Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        DIC;\n\n        tolerance       1e-8;\n        relTol          0.01;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda|h)\"\n    {\n        solver          PBiCGStab;\n        preconditioner  DILU;\n        tolerance       1e-10;\n        relTol          0.1;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-6;\n        U               1e-5;\n        \"(k|omega|epsilon|nuTilda|h)\"   1e-5;\n    }\n\n    nNonOrthogonalCorrectors 0;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n        rho             0.01;\n    }\n\n    equations\n    {\n        U               0.7;\n        h               0.7;\n        \"(k|omega|epsilon|nuTilda)\"     0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/residuals": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    For specified fields, writes out the initial residuals for the first\n    solution of each time step; for non-scalar fields (e.g. vectors), writes\n    the largest of the residuals for each component (e.g. x, y, z).\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/numerical/residuals.cfg\"\n\nfields (p U e k omega);\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndomain\n{\n    xMax  100;\n    zMax  50;\n\n    xMin #neg $xMax;\n    zMin #neg $zMax;\n\n    // Number of cells\n    zCells  60; // aerofoil to far field\n    xUCells 60; // upstream\n    xMCells 25; // middle\n    xDCells 50; // downstream\n\n    // Mesh grading\n    zGrading    300;  // aerofoil to far field\n    xUGrading   10;     // towards centre upstream\n    leadGrading 0.005;  // towards leading edge\n    xDGrading   400;    // downstream\n}\n\naerofoil\n{\n    xLead   0;\n    zLead   0;\n    xTrail  1;\n    zTrail  0;\n    xUpper  0.3;\n    zUpper  0.06;\n\n    xLower  $xUpper;\n    zLower  #neg $zUpper;\n}\n\ngeometry\n{\n    aerofoil\n    {\n        type   triSurface;\n        file   \"NACA0012.obj\";\n    }\n    cylinder\n    {\n        type   cylinder;\n        point1 ($!aerofoil/xUpper -1e3 0);\n        point2 ($!aerofoil/xUpper  1e3 0);\n        radius $!domain/zMax;\n    }\n}\n\nvertices\n(\n    project ($aerofoil/xLower -0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail -0.1 $domain/zMin)\n    ($domain/xMax -0.1 $domain/zMin)\n\n    project ($domain/xMin     -0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead  -0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax -0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower -0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper -0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper -0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail -0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax -0.1 $domain/zMax)\n\n    project ($aerofoil/xLower  0.1 $domain/zMin) (cylinder)\n    ($aerofoil/xTrail  0.1 $domain/zMin)\n    ($domain/xMax 0.1 $domain/zMin)\n\n    project ($domain/xMin      0.1 $aerofoil/zLead) (cylinder)\n    project ($aerofoil/xLead   0.1 $aerofoil/zLead) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $aerofoil/zTrail) (aerofoil)\n    ($domain/xMax 0.1 $aerofoil/zTrail)\n\n    project ($aerofoil/xLower  0.1 $aerofoil/zLower) (aerofoil)\n    project ($aerofoil/xUpper  0.1 $aerofoil/zUpper) (aerofoil)\n\n    project ($aerofoil/xUpper  0.1 $domain/zMax) (aerofoil)\n    project ($aerofoil/xTrail  0.1 $domain/zMax) (aerofoil)\n    ($domain/xMax 0.1 $domain/zMax)\n);\n\nblocks\n(\n    hex ( 7 4 16 19 0 3 15 12)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 5 7 19 17 1 0 12 13)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 17 18 6 5 13 14 2 1)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n\n    hex ( 20 16 4 8 21 15 3 9)\n    ($!domain/xUCells 1 $!domain/zCells)\n    edgeGrading\n    (\n        $!domain/leadGrading $!domain/leadGrading $!domain/xUGrading $!domain/xUGrading\n        1 1 1 1\n        $!domain/zGrading $!domain/zGrading $!domain/zGrading $!domain/zGrading\n    )\n\n    hex ( 17 20 8 5 22 21 9 10)\n    ($!domain/xMCells 1 $!domain/zCells)\n    simpleGrading (1 1 $!domain/zGrading)\n\n    hex ( 5 6 18 17 10 11 23 22)\n    ($!domain/xDCells 1 $!domain/zCells)\n    simpleGrading ($!domain/xDGrading 1 $!domain/zGrading)\n);\n\nedges\n(\n\n    project 4 7 (aerofoil)\n    project 7 5 (aerofoil)\n    project 4 8 (aerofoil)\n    project 8 5 (aerofoil)\n\n    project 16 19 (aerofoil)\n    project 19 17 (aerofoil)\n    project 16 20 (aerofoil)\n    project 20 17 (aerofoil)\n\n    project 3 0 (cylinder)\n    project 3 9 (cylinder)\n    project 15 12 (cylinder)\n    project 15 21 (cylinder)\n);\n\nboundary\n(\n    aerofoil\n    {\n        type wall;\n        faces\n        (\n            (4 7 19 16)\n            (7 5 17 19)\n            (5 8 20 17)\n            (8 4 16 20)\n        );\n    }\n\n    inlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (3 0 12 15)\n            (0 1 13 12)\n            (1 2 14 13)\n            (11 10 22 23)\n            (10 9 21 22)\n            (9 3 15 21)\n        );\n    }\n\n    outlet\n    {\n        type patch;\n        inGroups (freestream);\n        faces\n        (\n            (2 6 18 14)\n            (6 11 23 18)\n        );\n    }\n\n    back\n    {\n        type empty;\n        faces\n        (\n            (3 4 7 0)\n            (7 5 1 0)\n            (5 6 2 1)\n            (3 9 8 4)\n            (9 10 5 8)\n            (10 11 6 5)\n        );\n    }\n\n    front\n    {\n        type empty;\n        faces\n        (\n            (15 16 19 12)\n            (19 17 13 12)\n            (17 18 14 13)\n            (15 16 20 21)\n            (20 17 22 21)\n            (17 18 23 22)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/extrudeMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      extrudeMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconstructFrom patch;\nsourceCase \"$FOAM_CASE\";\n\nsourcePatches (back);\nexposedPatchName front;\n\nextrudeModel  plane;\nthickness     1;\n\nflipNormals false;\nmergeFaces false;\n\n// ************************************************************************* //\n",
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnuTildaInlet    1e-4;\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform $nuTildaInlet;\n\nboundaryField\n{\n    freestream\n    {\n        type            freestream;\n        freestreamValue uniform $nuTildaInlet;\n    }\n\n    wall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n"
+  },
+  "drivaerFastback/1": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. DrivAer fastback baseline at 100 km/h with static ground, rotatingWallVelocity wheels, and kOmegaSST. Set Uinlet to 27.7778 m/s. Use lightweight snappy mesh level 2. Run from t=0 to t=100; deltaT=1; write results every 50 using writeControl=timeStep. Enable forceCoeffs for aerodynamic coefficients. Keep geometry referenced by DrivAer body/frontWheels/rearWheels triSurface names without embedding solver results. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/2": {
+    "usr_requirement": "Run the supplied DrivAer fastback surrogate with foamRun -solver incompressibleFluid at the baseline 27.7778 m/s, but use a 60-cell streamwise background mesh instead of 40 cells. Keep static ground, rotatingWallVelocity wheels, kOmegaSST, forceCoeffs, and run controls unchanged; this is the medium-resolution variant. For Q2 evidence, continue the validated decomposed run to t=200 and merge restart-segment forceCoeffs history. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh -meshQuality -skewThreshold 11\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells 60;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\n\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         200;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n\n// The connected 60-cell mesh contains three faces at skewness 10.64.\nmaxInternalSkewness 11;\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (1 1);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (1 1);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels ((0.2 2));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/3": {
+    "usr_requirement": "Run the supplied DrivAer fastback surrogate with foamRun -solver incompressibleFluid using the baseline Uinlet=27.7778 m/s and an 80-cell streamwise background mesh. Keep static ground, rotatingWallVelocity wheels, kOmegaSST, forceCoeffs, and run controls unchanged. This is the fine-mesh third level after the 40-cell baseline and 60-cell variant. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh -meshQuality -skewThreshold 4.5\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells 80;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n\n// The 80-cell background mesh produces two benign 4.20-skew faces.\nmaxInternalSkewness 4.5;\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/4": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the vehicle speed to 120 km/h relative to the Fastback baseline. Set Uinlet to 33.3333 m/s and compute wheelSpeed from Uinlet/wheelRadius; keep the fastback geometry, static ground, rotatingWallVelocity wheels, snappy mesh, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          33.3333;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/5": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the vehicle speed to 80 km/h relative to the Fastback baseline. Set Uinlet to 22.2222 m/s and compute wheelSpeed from Uinlet/wheelRadius; keep the fastback geometry, static ground, rotatingWallVelocity wheels, snappy mesh, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          22.2222;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/6": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the wheel-rotation method to an MRF-style treatment for the front and rear wheels, while keeping the fastback geometry, 100 km/h inflow, static ground, mesh setup, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel topoSet\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            noSlip;\n    }\n\n    rearWheels\n    {\n        type            noSlip;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ],
+    "constant/MRFProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      MRFProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfrontWheelMRF\n{\n    cellZone    frontWheelZone;\n    origin      (0 0 0.318);\n    axis        (0 -1 0);\n    omega       87.3516;\n}\n\nrearWheelMRF\n{\n    cellZone    rearWheelZone;\n    origin      (2.786 0 0.318);\n    axis        (0 -1 0);\n    omega       87.3516;\n}\n\n// ************************************************************************* //\n",
+    "system/topoSetDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      topoSetDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nactions\n(\n    {\n        name    frontWheelCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (-0.5 -1.2 0.0) (0.8 1.2 0.8);\n    }\n    {\n        name    frontWheelZone;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     frontWheelCells;\n    }\n    {\n        name    rearWheelCells;\n        type    cellSet;\n        action  new;\n        source  boxToCell;\n        box     (2.2 -1.2 0.0) (3.4 1.2 0.8);\n    }\n    {\n        name    rearWheelZone;\n        type    cellZoneSet;\n        action  new;\n        source  setToCellZone;\n        set     rearWheelCells;\n    }\n);\n\n// ************************************************************************* //\n"
+  },
+  "drivaerFastback/7": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the ground boundary condition to a moving ground with velocity Uinlet, while keeping the fastback geometry, 100 km/h inflow, rotatingWallVelocity wheels, mesh setup, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/8": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Use the standard kEpsilon turbulence model, while keeping the fastback geometry, 100 km/h inflow, wheel treatment, mesh setup, run controls, and forceCoeffs post-processing consistent with the baseline. For Q2 evidence, continue the validated decomposed run to t=200 and merge restart-segment forceCoeffs history. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/epsilon": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      epsilon;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nepsilonInlet    0.02;\n\ndimensions      [0 2 -3 0 0 0 0];\n\ninternalField   uniform $epsilonInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $epsilonInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $epsilonInlet;\n        value           uniform $epsilonInlet;\n    }\n\n    wall\n    {\n        type            epsilonWallFunction;\n        value           uniform $epsilonInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $epsilonInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutkWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kEpsilon;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format          ascii;\n    class           dictionary;\n    object          controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\n\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         200;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/9": {
+    "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Use the standard RAS kOmega turbulence model instead of the baseline kOmegaSST model, while keeping the fastback geometry, 100 km/h inflow, wheel treatment, mesh setup, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType RAS;\n\nRAS\n{\n    model               kOmega;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         100;\n\ndeltaT          1;\n\nwriteControl    timeStep;\n\nwriteInterval   50;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         steadyState;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nSIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ]
+  },
+  "drivaerFastback/10": {
+    "usr_requirement": "Perform a transient 3D DrivAer fastback DDES benchmark using foamRun -solver incompressibleFluid with LES SpalartAllmarasDDES, Euler time discretisation, PIMPLE coupling, Uinlet=27.7778 m/s, rotating wheels, static ground, and the supplied geometry. Use endTime=10, deltaT=0.01, writeControl=timeStep, and writeInterval=10; analyse the final transient window rather than treating this as a steady simpleFoam run. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\n\nusage () {\n    exec 1>&2\n    while [ \"$#\" -ge 1 ]; do echo \"$1\"; shift; done\n    cat <<USAGE\n\nUsage: ${0##*/} [OPTIONS]\noptions:\n  -c | -cores <nCores>   number of cores in parallel run\n  -h | -help             help\n  -m | -mesh <S|M|L|XL>  mesh size\n                         - S: small, 440k cells\n                         - M: medium, 3M cells (default)\n                         - L: large, 22.5M cells\n                         - XL: extra large, ~200M cells\n\nRuns the ${PWD##*/} simulation\n\nUSAGE\n    exit 1\n}\n\ncheckCores () {\n    _cores=\"$1\"\n\n    ! [ \"$_cores\" -eq \"$_cores\" ] 2> /dev/null && \\\n        echo \"Number of cores '$_cores' must be an integer\" && \\\n        return 1\n\n    [ \"$_cores\" -lt 2 ] && \\\n        echo \"Number of cores '$_cores' must be >= 2\" && \\\n        return 1\n\n    return 0\n}\n\nrefineBackgroundMesh () {\n    _nRefine=\"$1\"\n    _r=0\n    while [ $_r -lt \"$_nRefine\" ]\n    do\n        echo \"Refining the background mesh\"\n        runParallel -a refineMesh -all\n        _r=$(( _r + 1 ))\n    done\n}\n\nsetKeyword () {\n    _entry=\"$1\"\n    _value=\"$2\"\n    _file=\"$3\"\n\n    foamDictionary -entry \"$_entry\" -set \"$_value\" \"$_file\" > /dev/null\n}\n\nnRefine=1\nnCores=8\n\nwhile [ \"$#\" -gt 0 ]\ndo\n   case \"$1\" in\n   -c | -cores)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      nCores=$2\n      shift 2\n      checkCores \"$nCores\" || usage\n      setKeyword numberOfSubdomains \"$nCores\" system/decomposeParDict\n      ;;\n   -h | -help)\n      usage\n      ;;\n   -m | -mesh)\n      [ \"$#\" -ge 2 ] || usage \"'$1' option requires an argument\"\n      mesh=$2\n      shift 2\n      case \"$mesh\" in\n          S)  nRefine=0 ;;\n          M)  ;;\n          L)  nRefine=2 ; setKeyword endTime 2000 system/controlDict ;;\n          XL) nRefine=3 ; setKeyword endTime 2000 system/controlDict ;;\n          *)  usage \"Invalid argument '$mesh' to -m|-mesh <S|M|L|XL>.\" ;;\n      esac\n      ;;\n   -test)\n      shift\n      ;;\n   -*)\n      usage \"Invalid option '$1'\"\n      ;;\n   *)\n      break\n      ;;\n    esac\ndone\n\n# START OF MAIN SCRIPT\n\nrunApplication blockMesh\n\nrunApplication decomposePar -copyZero\n\nrefineBackgroundMesh $nRefine\n\nrunParallel snappyHexMesh\n\nrunParallel checkMesh\n\nrunParallel foamRun -solver incompressibleFluid\n\n# runApplication reconstructPar -latestTime\n\n#------------------------------------------------------------------------------\n",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nUinlet          27.7778;\n\nwheelRadius     0.318;\nwheelBase       2.786;\nwheelSpeed      #calc \"$Uinlet / $wheelRadius\";\n\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform ($Uinlet 0 0);\n    }\n\n    ground\n    {\n        type            noSlip;\n    }\n\n    freestream\n    {\n        type            freestreamVelocity;\n        freestreamValue uniform ($Uinlet 0 0);\n    }\n\n    wall\n    {\n        type            noSlip;\n    }\n\n    frontWheels\n    {\n        type            rotatingWallVelocity;\n        origin          (0 0 $wheelRadius);\n        axis            (0 -1 0);\n        omega           $wheelSpeed;\n    }\n\n    rearWheels\n    {\n        $frontWheels;\n        origin          ($wheelBase 0 $wheelRadius);\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform (0 0 0);\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            zeroGradient;\n    }\n\n    freestream\n    {\n        type            freestreamPressure;\n        freestreamValue uniform 0;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            zeroGradient;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/k": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      k;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nkInlet          0.002;\n\ndimensions      [0 2 -2 0 0 0 0];\n\ninternalField   uniform $kInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $kInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $kInlet;\n        value           uniform $kInlet;\n    }\n\n    wall\n    {\n        type            kqRWallFunction;\n        value           uniform $kInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $kInlet;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/omega": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      omega;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nomegaInlet      1.0;\n\ndimensions      [0 0 -1 0 0 0 0];\n\ninternalField   uniform $omegaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $omegaInlet;\n    }\n\n    freestream\n    {\n        type            inletOutlet;\n        inletValue      uniform $omegaInlet;\n        value           uniform $omegaInlet;\n    }\n\n    wall\n    {\n        type            omegaWallFunction;\n        value           uniform $omegaInlet;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $omegaInlet;\n    }\n\n    #includeEtc \"caseDicts/setConstraintTypes\"\n}\n\n// ************************************************************************* //\n",
+    "0/nut": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nut;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    inlet\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    freestream\n    {\n        type            calculated;\n        value           uniform 0;\n    }\n\n    wall\n    {\n        type            nutUSpaldingWallFunction;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform 0;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType LES;\n\nRAS\n{\n    model               kOmegaSST;\n\n    turbulence          on;\n}\n\nLES\n{\n    model               SpalartAllmarasDDES;\n    delta               cubeRootVol;\n\n    turbulence          on;\n\n    cubeRootVolCoeffs\n    {\n        deltaCoeff      1;\n    }\n\n    smoothCoeffs\n    {\n        delta           cubeRootVol;\n        cubeRootVolCoeffs\n        {\n            deltaCoeff      1;\n        }\n        maxDeltaRatio   1.1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nviscosityModel  constant;\n\nnu              [0 2 -1 0 0 0 0] 1.5e-05;\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nxMin   -10;\nxMax    30;\nyMin   -5;\nyMax    5;\nzMin    0;\nzMax    8;\nxCells  40;\nyCells  10;\nzCells  8;\n\nconvertToMeters 1;\n\nvertices\n(\n    ($xMin $yMin $zMin)\n    ($xMax $yMin $zMin)\n    ($xMax $yMax $zMin)\n    ($xMin $yMax $zMin)\n\n    ($xMin $yMin $zMax)\n    ($xMax $yMin $zMax)\n    ($xMax $yMax $zMax)\n    ($xMin $yMax $zMax)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) ($xCells $yCells $zCells) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    inlet\n    {\n        type patch;\n        faces\n        (\n            (0 3 7 4)\n        );\n    }\n\n    freestream\n    {\n        type patch;\n        faces\n        (\n            (1 5 6 2)\n            (4 7 6 5)\n            (3 2 6 7)\n            (0 4 5 1)\n        );\n    }\n\n    ground\n    {\n        type wall;\n        faces\n        (\n            (0 1 2 3)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\napplication     foamRun;\nsolver          incompressibleFluid;\n\nstartFrom       latestTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         10;\n\ndeltaT          0.01;\n\nwriteControl    timeStep;\n\nwriteInterval   10;\n\npurgeWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision   8;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\n// adjustTimeStep  yes;\n\n// maxCo           1;\n\n\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains  8;\n\nmethod              scotch;\n//method              hierarchical;\n\nhierarchicalCoeffs\n{\n    n               (4 2 1);\n    order           xyz;\n}\n\n// ************************************************************************* //\n",
+    "system/forceCoeffsIncompressible": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n-------------------------------------------------------------------------------\nDescription\n    Calculates lift, drag and moment coefficients by summing forces on\n    specified patches for a case where the solver is incompressible; i.e.,\n    pressure is kinematic and has units of m^2/s^2.\n\n\\*---------------------------------------------------------------------------*/\n\n#includeEtc \"caseDicts/functions/forces/forceCoeffsIncompressible.cfg\"\n\n#include    \"$FOAM_CASE/0/U\"\n\npatches     (\".*(body|Wheels)\"); // Patches on which to calculate forces\n\nmagUInf     $Uinlet;        // Far field velocity magnitude; e.g., 20 m/s\nlRef        $wheelBase;     // Reference length scale for moment calculations;\n                            // e.g., 1 m\nAref        2.154;          // Reference area; e.g., 1 m^2\n\nCofR        (1.391 0 0);    // Centre of rotation; e.g., (0 0 0)\n\nliftDir     (0 0 1);        // Direction of lift force; e.g., (0 0 1)\ndragDir     (1 0 0);        // Direction of drag force; e.g., (1 0 0)\npitchAxis   (0 1 0);        // Pitch axis; e.g., (0 1 0)\n\n// ************************************************************************* //\n",
+    "system/functions": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      functions;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeFunc forceCoeffsIncompressible\n\n#includeFunc time\n\n#includeFunc streamlinesSphere\n(\n    name=streamlines,\n    centre=(4 0 0.7),\n    radius=1,\n    nPoints=30,\n    fields=(U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=xNormal,\n    point=(4 0 1),\n    normal=(1 0 0),\n    fields=(p U)\n)\n\n#includeFunc cutPlaneSurface\n(\n    name=yNormal,\n    point=(-5 0.02 1),\n    normal=(0 1 0),\n    fields=(p U)\n)\n\n#includeFunc patchSurface(name=car, patch=\".*(body|Wheels)\", p)\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nddtSchemes\n{\n    // For transient, replace steadyState, e.g. with Euler\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n\n    limited         cellLimited Gauss linear 1;\n    grad(U)         $limited;\n    grad(k)         $limited;\n    grad(omega)     $limited;\n}\n\ndivSchemes\n{\n    default         none;\n\n    // For transient, remove \"bounded\"\n    div(phi,U)      bounded Gauss linearUpwind limited;\n\n    // For transient, remove \"bounded\"\n    turbulence      bounded Gauss limitedLinear 1;\n    div(phi,k)      $turbulence;\n    div(phi,omega)  $turbulence;\n    div(phi,epsilon) $turbulence;\n    div(phi,nuTilda) $turbulence;\n\n    div((nuEff*dev2(T(grad(U))))) Gauss linear;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear corrected;\n}\n\ninterpolationSchemes\n{\n    default         linear;\n}\n\nsnGradSchemes\n{\n    default         corrected;\n}\n\nwallDist\n{\n    method meshWave;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    p\n    {\n        solver          GAMG;\n        smoother        GaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    pFinal\n    {\n        $p;\n        relTol         0;\n    }\n\n    Phi\n    {\n        $p;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda)\"\n    {\n        solver          smoothSolver;\n        smoother        symGaussSeidel;\n        tolerance       1e-6;\n        relTol          0.1;\n    }\n\n    \"(U|k|omega|epsilon|nuTilda)Final\"\n    {\n        $U;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    residualControl\n    {\n        p               1e-4;\n        U               1e-4;\n        \"(k|omega|epsilon|nuTilda)\" 1e-4;\n    }\n    nNonOrthogonalCorrectors 0;\n    pRefCell        0;\n    pRefValue       0;\n\n}\n\npotentialFlow\n{\n    nNonOrthogonalCorrectors 10;\n}\n\nrelaxationFactors\n{\n    fields\n    {\n        p               0.3;\n    }\n    equations\n    {\n        U               0.7;\n        \"(k|omega|epsilon|nuTilda)\" 0.7;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/meshQualityDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      meshQualityDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/meshQualityDict.cfg\"\n\n//- minFaceWeight (0 -> 0.5)\n//minFaceWeight 0.02;\n\n// ************************************************************************* //\n",
+    "system/snappyHexMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      snappyHexMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\n#includeEtc \"caseDicts/mesh/generation/snappyHexMeshDict.cfg\"\n\ncastellatedMesh on;\nsnap            on;\naddLayers       off;\n\ngeometry\n{\n    body\n    {\n        type triSurface;\n        file \"body.obj\";\n    }\n\n    frontWheels\n    {\n        type triSurface;\n        file \"frontWheels.obj\";\n    }\n\n    rearWheels\n    {\n        type triSurface;\n        file \"rearWheels.obj\";\n    }\n\n    upstream\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.8);\n    }\n\n    underbody\n    {\n        type box;\n        min (-10 -1.5  0);\n        max ( 3   1.5  0.15);\n    }\n\n    wake\n    {\n        type box;\n        min ( 3 -1.2  0);\n        max ( 6  1.2 1.4);\n    }\n\n    downstream\n    {\n        type box;\n        min ( 3 -1.5  0);\n        max (30  1.5 1.8);\n    }\n};\n\ncastellatedMeshControls\n{\n    features ();\n\n    refinementSurfaces\n    {\n        body\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n\n        \".*Wheels\" // level 5 needed to avoid single cells in treads\n        {\n            level (2 2);\n            patchInfo { type wall; }\n        }\n    }\n\n    refinementRegions\n    {\n        body\n        {\n            mode    distance;\n            levels  ((0.2 3));\n        }\n\n        \"(wake|underbody)\"\n        {\n            mode    inside;\n            level   2;\n        }\n\n        \".*stream\"\n        {\n            mode    inside;\n            level   1;\n        }\n    }\n\n    insidePoint (0 0 3);\n    nCellsBetweenLevels 5;\n}\n\nsnapControls\n{\n    nSmoothPatch 5;\n    tolerance 1.5;\n    nSolveIter 20;\n    nRelaxIter 8;\n    nFeatureSnapIter 0;\n    implicitFeatureSnap false;\n    explicitFeatureSnap false;\n    multiRegionFeatureSnap false;\n}\n\naddLayersControls\n{\n    layers\n    {\n        body\n        {\n            nSurfaceLayers 2;\n        }\n    }\n\n    relativeSizes       on;\n    expansionRatio      1.2;\n    finalLayerThickness 0.5;\n    minThickness        1e-3;\n    maxThicknessToMedialRatio 0.6;\n}\n\nwriteFlags ();\n\nmergeTolerance 1e-6;\n\n// ************************************************************************* //\n",
+    "_external_assets": [
+      {
+        "asset_id": "drivaerFastback/body",
+        "target": "constant/geometry/body.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/frontWheels",
+        "target": "constant/geometry/frontWheels.obj.gz"
+      },
+      {
+        "asset_id": "drivaerFastback/rearWheels",
+        "target": "constant/geometry/rearWheels.obj.gz"
+      }
+    ],
+    "0/nuTilda": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      nuTilda;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnuTildaInlet    1e-5;\n\ndimensions      [0 2 -1 0 0 0 0];\n\ninternalField   uniform $nuTildaInlet;\n\nboundaryField\n{\n    inlet\n    {\n        type            fixedValue;\n        value           uniform $nuTildaInlet;\n    }\n\n    freestream\n    {\n        type            freestream;\n        freestreamValue uniform $nuTildaInlet;\n        value           uniform $nuTildaInlet;\n    }\n\n    wall\n    {\n        type            fixedValue;\n        value           uniform 0;\n    }\n\n    processor\n    {\n        type            processor;\n        value           uniform $nuTildaInlet;\n    }\n}\n\n// ************************************************************************* //\n"
+  },
+  "riemann2D/1": {
+    "usr_requirement": "Configure and run the CFD-China four-quadrant two-dimensional Riemann problem in OpenFOAM-13 using foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use the square domain [-5,5] x [-5,5] on a uniform 800 x 800 mesh with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov central-upwind flux, vanAlbada reconstruction for rho and T, and vanAlbadaV reconstruction for U. Use zero-gradient conditions on the four outer sides and empty front/back patches. Advance to t=1.5 with adaptive time stepping and maxCo=0.2, writing results every 0.15 time units. Provide time-resolved density and pressure contours together with final rho and p profiles along the horizontal and vertical centre-lines.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n\n\n// ************************************************************************* //\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (800 800 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT          2e-4;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 4;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)  vanAlbadaV;\n    reconstruct(T)  vanAlbada;\n\n    flux(rhoU)      linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\n\ninterpolationScheme cellPoint;\n\nsetFormat       raw;\n\nsets\n{\n    horizontal\n    {\n        type    lineFace;\n        axis    x;\n        start   (-4.995 0 0);\n        end     (4.995 0 0);\n        nPoints 400;\n    }\n\n    vertical\n    {\n        type    lineFace;\n        axis    y;\n        start   (0 -4.995 0);\n        end     (0 4.995 0);\n        nPoints 400;\n    }\n}\n\nfields          (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\\\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\\\    /   O peration     | Website:  https://openfoam.org\n    \\\\  /    A nd           | Version:  13\n     \\\\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type        box;\n        zoneType    cell;\n        zoneType    cell;\n        box         (-100 -100 -2) (0 0 2);\n\n        values\n        {\n            U       (1.206 1.206 0);\n            p       0.029;\n            T       0.294220591773;\n        }\n    }\n\n    southEast\n    {\n        type        box;\n        zoneType    cell;\n        zoneType    cell;\n        box         (0 -100 -2) (100 0 2);\n\n        values\n        {\n            U       (0 1.206 0);\n            p       0.3;\n            T       0.789076195003;\n        }\n    }\n\n    northWest\n    {\n        type        box;\n        zoneType    cell;\n        zoneType    cell;\n        box         (-100 0 -2) (0 100 2);\n\n        values\n        {\n            U       (1.206 0 0);\n            p       0.3;\n            T       0.789076195003;\n        }\n    }\n\n    northEast\n    {\n        type        box;\n        zoneType    cell;\n        zoneType    cell;\n        box         (0 0 -2) (100 100 2);\n\n        values\n        {\n            U       (0 0 0);\n            p       1.5;\n            T       1.40008419533;\n        }\n    }\n}\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd ${0%/*} || exit 1    # Run from this directory\n\n# Source tutorial run functions\n. $WM_PROJECT_DIR/bin/tools/RunFunctions\n\nrunApplication blockMesh\nrunApplication setFields\nrunApplication decomposePar\nrunParallel foamRun -solver shockFluid\nrunApplication reconstructPar -latestTime\nrunApplication -s sample foamPostProcess -latestTime -func sample\n\n#------------------------------------------------------------------------------\n"
+  },
+  "riemann2D/2": {
+    "usr_requirement": "Perform a spatial-convergence study of the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use the square domain [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov central-upwind flux, vanAlbada reconstruction for rho and T, and vanAlbadaV reconstruction for U. Use zero-gradient conditions on the four outer sides and empty front/back patches. Advance to t=1.5 with adaptive time stepping and maxCo=0.2, writing results every 0.15 time units. Run otherwise identical uniform 200 x 200, 400 x 400 and 800 x 800 meshes, with outputs at the same physical times. Compare the density and pressure fields and centre-line profiles across the three resolutions, and discuss the observed convergence behaviour in smooth regions and across shocks and contact discontinuities.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (200 200 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 200;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 200;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy spatial_convergence;\nmeshSizes (200 400 800);\ndomain (-5 -5) (5 5);\ncommonSamplingMesh 200;\noutputTimes (0.15 0.3 0.45 0.6 0.75 0.9 1.05 1.2 1.35 1.5);\nmetrics (rho_L1 rho_L2 p_L1 p_L2 shockThicknessCells shockThicknessDistance massDrift energyDrift);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch grid_200\n(cd grid_200 && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch grid_400\n(cd grid_400 && sed -i \"s/(200 200 1)/(400 400 1)/\" system/blockMeshDict && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch grid_800\n(cd grid_800 && sed -i \"s/(200 200 1)/(800 800 1)/\" system/blockMeshDict && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_grids.py grid_200 grid_400 grid_800\n",
+    "system/compare_grids.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'grid-convergence', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/3": {
+    "usr_requirement": "Assess Courant-number sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a fixed uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov flux with vanAlbada reconstruction for rho and T and vanAlbadaV for U, with zero-gradient outer boundaries. Run otherwise identical adaptive-time-step branches with maxCo=0.1 and maxCo=0.2 to t=1.5, writing both at the same physical times every 0.15. Compare their density and pressure fields, centre-line profiles, wave positions and computational effort.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.1;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy courant_sensitivity;\nmesh (600 600 1);\nmaxCoBranches (0.1 0.2);\noutputTimes (0.15 0.3 0.45 0.6 0.75 0.9 1.05 1.2 1.35 1.5);\nreferenceBranch maxCo_0p1;\nmetrics (stepCount wallClock minRhoHistory minPHistory centerlineL1);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch maxCo_0p1\n(cd maxCo_0p1 && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch maxCo_0p2\n(cd maxCo_0p2 && sed -i \"s/maxCo           0.1/maxCo           0.2/\" system/controlDict && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_courant.py maxCo_0p1 maxCo_0p2\n",
+    "system/compare_courant.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef full_field_minima(root):\n    path = root / \"postProcessing\" / \"extrema\" / \"0\" / \"volFieldValue.dat\"\n    rows = []\n    if path.is_file():\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            if len(values) >= 4: rows.append(values[:4])\n    return rows[-1][1:] if rows else []\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    extrema = full_field_minima(root)\n    sample_positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    full_field_positive = len(extrema) == 3 and all(math.isfinite(x) and x > 0 for x in extrema)\n    positive = sample_positive and full_field_positive\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"samplePositive\": sample_positive,\n            \"fullFieldPositive\": full_field_positive,\n            \"minRho\": extrema[0] if len(extrema) == 3 else (min(rho) if rho else None),\n            \"minP\": extrema[1] if len(extrema) == 3 else (min(p) if p else None),\n            \"minT\": extrema[2] if len(extrema) == 3 else (min(temp) if temp else None),\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'courant-sensitivity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/4": {
+    "usr_requirement": "Compare the Kurganov and Tadmor central fluxes for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use vanAlbada reconstruction for rho and T and vanAlbadaV for U, zero-gradient outer boundaries, adaptive stepping with maxCo=0.2, and run to t=1.5 with outputs every 0.15. Change only the flux formulation between the two branches, and compare their density and pressure fields, centre-line profiles, discontinuity resolution, numerical oscillations, robustness and computational cost.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy flux_sensitivity;\nfluxBranches (Kurganov Tadmor);\nmesh (600 600 1);\nmaxCo 0.2;\nmetrics (rhoContour pContour centerline extrema positivity shockThickness massDrift energyDrift runtime rho_L1);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch flux_Kurganov\n(cd flux_Kurganov && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch flux_Tadmor\n(cd flux_Tadmor && sed -i \"s/fluxScheme      Kurganov/fluxScheme      Tadmor/\" system/fvSchemes && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_flux.py flux_Kurganov flux_Tadmor\n",
+    "system/compare_flux.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'flux-sensitivity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/5": {
+    "usr_requirement": "Assess reconstruction-limiter sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Retain the Kurganov flux, zero-gradient outer boundaries, adaptive stepping with maxCo=0.2 and an end time of 1.5 with outputs every 0.15. Compare a vanAlbada/vanAlbadaV branch against a vanLeer/vanLeerV branch, changing only the reconstruction limiter. Compare density and pressure fields and centre-line profiles, with attention to discontinuity sharpness, post-shock oscillations and robustness.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy reconstruction_sensitivity;\nlimiterBranches (vanAlbada vanLeer);\nmesh (600 600 1);\nfluxScheme Kurganov;\nmetrics (centerline waveLocation shockThickness overshoot undershoot minRho minP massDrift energyDrift runtime);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch limiter_vanAlbada\n(cd limiter_vanAlbada && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch limiter_vanLeer\n(cd limiter_vanLeer && sed -i \"s/vanAlbada/vanLeer/g; s/vanAlbadaV/vanLeerV/g\" system/fvSchemes && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_limiters.py limiter_vanAlbada limiter_vanLeer\n",
+    "system/compare_limiters.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'limiter-sensitivity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/6": {
+    "usr_requirement": "Evaluate mesh-orientation bias for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 Cartesian mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Run a baseline branch and a second branch in which the initial discontinuity geometry is rotated by 45 degrees while the mesh remains fixed. Define x'=(x+y)/sqrt(2) and y'=(-x+y)/sqrt(2), assign the same four states according to the signs of x' and y', and rotate their velocity vectors consistently into the physical x-y frame. Use the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries and maxCo=0.2, and run both branches to t=1.5 with outputs every 0.15. Rotate the second result back to the baseline frame and compare the density and pressure fields on the common interior [-3.5,3.5] x [-3.5,3.5].",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-3.495 0 0); end (3.495 0 0); nPoints 420;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -3.495 0); end (0 3.495 0); nPoints 420;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultFieldValues\n(\n    volVectorFieldValue U (0 0 0)\n    volScalarFieldValue p 1.5\n    volScalarFieldValue T 1.40008419533\n);\n\nregions\n(\n    rotatedBoxToCell\n    {\n        origin (0 0 -2); i (5 5 0); j (-5 5 0); k (0 0 4);\n        fieldValues\n        (\n            volVectorFieldValue U (0 0 0)\n            volScalarFieldValue p 1.5\n            volScalarFieldValue T 1.40008419533\n        );\n    }\n    rotatedBoxToCell\n    {\n        origin (-5 -5 -2); i (5 5 0); j (-5 5 0); k (0 0 4);\n        fieldValues\n        (\n            volVectorFieldValue U (0.852770027 0.852770027 0)\n            volScalarFieldValue p 0.3\n            volScalarFieldValue T 0.789076195003\n        );\n    }\n    rotatedBoxToCell\n    {\n        origin (5 -5 -2); i (5 5 0); j (-5 5 0); k (0 0 4);\n        fieldValues\n        (\n            volVectorFieldValue U (-0.852770027 0.852770027 0)\n            volScalarFieldValue p 0.3\n            volScalarFieldValue T 0.789076195003\n        );\n    }\n    rotatedBoxToCell\n    {\n        origin (0 -10 -2); i (5 5 0); j (-5 5 0); k (0 0 4);\n        fieldValues\n        (\n            volVectorFieldValue U (0 1.705540054 0)\n            volScalarFieldValue p 0.029\n            volScalarFieldValue T 0.294220591773\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/setFieldsBaselineDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy mesh_orientation;\nrotationAngle 45;\nxPrimeFormula \"(x+y)/sqrt(2)\"; yPrimeFormula \"(-x+y)/sqrt(2)\";\nmesh (600 600 1);\ncompareWith baselineFrame; comparisonInterior \"(-3.5 -3.5) (3.5 3.5)\";\nmetrics (rho_L1 rho_LInf p_L1 p_LInf waveOffset symmetryError minRho minP);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch baseline\n(cd baseline && cp system/setFieldsBaselineDict system/setFieldsDict && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch rotated\n(cd rotated && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_orientation.py baseline rotated\n",
+    "system/compare_orientation.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'orientation-bias', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/7": {
+    "usr_requirement": "Assess domain-size and outer-boundary sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use one cell through the empty direction in both domains. Use the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries and maxCo=0.2. Run a small domain [-2.5,2.5] x [-2.5,2.5] on a 300 x 300 mesh and a large domain [-5,5] x [-5,5] on a 600 x 600 mesh, so that both use the same spatial resolution. Advance both to t=1.5 and write at matched times every 0.15. Compare their flow fields on the common interior [-2,2] x [-2,2] and identify when and how the smaller outer boundary begins to affect the solution.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-2.5 -2.5 -1)\n    (2.5 -2.5 -1)\n    (2.5 2.5 -1)\n    (-2.5 2.5 -1)\n    (-2.5 -2.5 1)\n    (2.5 -2.5 1)\n    (2.5 2.5 1)\n    (-2.5 2.5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (300 300 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-1.995 0 0); end (1.995 0 0); nPoints 240;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -1.995 0); end (0 1.995 0); nPoints 240;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy domain_sensitivity;\nsmallDomain \"(-2.5 -2.5) (2.5 2.5)\"; largeDomain \"(-5 -5) (5 5)\";\nsmallMesh \"(300 300 1)\"; largeMesh \"(600 600 1)\";\ndelta 0.0166666666667; comparisonInterior \"(-2 -2) (2 2)\";\nmetrics (rho_L1 rho_LInf p_L1 p_LInf T_L1 U_L1 boundaryReflection centerlineDeviation massDrift energyDrift);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch domain_5\n(cd domain_5 && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch domain_10\n(cd domain_10 && sed -i \"s/-2.5 -2.5 -1/-5 -5 -1/; s/2.5 -2.5 -1/5 -5 -1/; s/2.5 2.5 -1/5 5 -1/; s/-2.5 2.5 -1/-5 5 -1/; s/-2.5 -2.5 1/-5 -5 1/; s/2.5 -2.5 1/5 -5 1/; s/2.5 2.5 1/5 5 1/; s/-2.5 2.5 1/-5 5 1/; s/(300 300 1)/(600 600 1)/\" system/blockMeshDict && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_domains.py domain_5 domain_10\n",
+    "system/compare_domains.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'domain-sensitivity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/8": {
+    "usr_requirement": "Stress-test positivity and nonlinear robustness for a strengthened four-quadrant two-dimensional Riemann interaction using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize (rho,p,u,v) as NE=(1.5,3.0,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.069,0.0145,1.206,1.206), and SE=(0.5323,0.3,0,1.206), deriving temperature consistently from the equation of state. Use the Kurganov flux, vanAlbada reconstruction for rho and T, vanAlbadaV for U, zero-gradient outer boundaries and adaptive stepping with maxCo=0.2. Attempt to reach t=1.5 without clipping, flooring or changing the stated physics. If the calculation fails, retain the failing configuration and identify the first failure time and affected field.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    timeStep;\n        writeInterval   1;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    timeStep;\n        writeInterval   1;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       3.0;\n    T       2.80016839067;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.0145; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 3.0; T 2.80016839067; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'strict-positivity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy positivity_robustness;\nmesh (600 600 1); maxCo 0.2; endTime 1.5;\nstates \"NE=(1.5 3.0 0 0); NW=(0.5323 0.3 1.206 0); SW=(0.069 0.0145 1.206 1.206); SE=(0.5323 0.3 0 1.206)\";\nmetrics (minRhoHistory minPHistory minTHistory nonFiniteRows failedSteps massDrift energyDrift waveExtrema);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\nrunApplication blockMesh\nrunApplication setFields\nrunApplication foamRun -solver shockFluid\nrunApplication -s sample foamPostProcess -latestTime -func sample\npython3 system/validateRiemann.py \"postProcessing\"\n"
+  },
+  "riemann2D/9": {
+    "usr_requirement": "Evaluate parallel-decomposition invariance and solver scaling for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use a uniform 800 x 800 mesh over [-5,5] x [-5,5] with one cell through the empty direction, the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries, maxCo=0.2 and an end time of 1.5 with outputs every 0.15. Execute matched serial, two-rank and four-rank runs, using scotch decomposition for the parallel branches. Compare the reconstructed final fields and centre-line profiles and report speedup and parallel efficiency. Measure elapsed time for the foamRun solver phase only, excluding mesh generation, initialization, decomposition, reconstruction, sampling and comparison.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (800 800 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy decomposition_invariance;\nbranches (serial twoRank fourRank); parallelMethod scotch;\nmesh (800 800 1); outputTimes (0.15 0.3 0.45 0.6 0.75 0.9 1.05 1.2 1.35 1.5);\ntimingScope foamRunOnly; metrics (cellCountBalance elapsedTime speedup parallelEfficiency rho_L1 rho_LInf p_L1 p_LInf T_L1 U_L1 centerline extrema massDrift energyDrift);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\n\nrun_branch() {\n    name=\"$1\"; shift\n    mkdir -p \"$name\"\n    cp -r 0 constant system \"$name\"/\n}\nrun_branch serial\n(cd serial && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch parallel_2\n(cd parallel_2 && sed -i \"s/numberOfSubdomains 1/numberOfSubdomains 2/\" system/decomposeParDict && runApplication blockMesh && runApplication setFields && runApplication decomposePar && runParallel foamRun -solver shockFluid && runApplication reconstructPar -latestTime && runApplication -s sample foamPostProcess -latestTime -func sample)\nrun_branch parallel_4\n(cd parallel_4 && sed -i \"s/numberOfSubdomains 1/numberOfSubdomains 4/\" system/decomposeParDict && runApplication blockMesh && runApplication setFields && runApplication decomposePar && runParallel foamRun -solver shockFluid && runApplication reconstructPar -latestTime && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_decompositions.py serial parallel_2 parallel_4\n",
+    "system/compare_decompositions.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'decomposition-invariance', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  },
+  "riemann2D/10": {
+    "usr_requirement": "Evaluate restart fidelity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use a uniform 600 x 600 mesh over [-5,5] x [-5,5] with one cell through the empty direction, the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries, adaptive stepping at maxCo=0.2 and a final time of 1.5 with outputs every 0.15. Run one branch continuously from t=0 to 1.5. Run a second branch from t=0 to 0.75, write a complete binary restart state, and continue from the latest saved time to t=1.5 without reinitializing the fields. Compare the final rho, p, T and U fields, both centre-line profiles, time-step histories and output-time alignment between the continuous and restarted runs.",
+    "0/U": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volVectorField;\n    location    \"0\";\n    object      U;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 1 -1 0 0 0 0];\n\ninternalField   uniform (0 0 0);\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/T": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      T;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [0 0 0 1 0 0 0];\n\ninternalField   uniform 1;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "0/p": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       volScalarField;\n    location    \"0\";\n    object      p;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndimensions      [1 -1 -2 0 0 0 0];\n\ninternalField   uniform 0;\n\nboundaryField\n{\n    sides\n    {\n        type            zeroGradient;\n    }\n\n    empty\n    {\n        type            empty;\n    }\n}\n\n// ************************************************************************* //\n",
+    "constant/momentumTransport": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      momentumTransport;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsimulationType  laminar;\n",
+    "constant/physicalProperties": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"constant\";\n    object      physicalProperties;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nthermoType\n{\n    type            hePsiThermo;\n    mixture         pureMixture;\n    transport       const;\n    thermo          hConst;\n    equationOfState perfectGas;\n    specie          specie;\n    energy          sensibleInternalEnergy;\n}\n\nmixture\n{\n    specie\n    {\n        molWeight       11640.3;\n    }\n    thermodynamics\n    {\n        Cp              2.5;\n        hf              0;\n    }\n    transport\n    {\n        mu              0;\n        Pr              1;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/blockMeshDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    \n    object      blockMeshDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nconvertToMeters 1;\n\nvertices\n(\n    (-5 -5 -1)\n    (5 -5 -1)\n    (5 5 -1)\n    (-5 5 -1)\n    (-5 -5 1)\n    (5 -5 1)\n    (5 5 1)\n    (-5 5 1)\n);\n\nblocks\n(\n    hex (0 1 2 3 4 5 6 7) (600 600 1) simpleGrading (1 1 1)\n);\n\nboundary\n(\n    sides\n    {\n        type patch;\n        faces\n        (\n            (1 2 6 5)\n            (0 4 7 3)\n            (0 1 5 4)\n            (3 7 6 2)\n        );\n    }\n    empty\n    {\n        type empty;\n        faces\n        (\n            (5 6 7 4)\n            (0 3 2 1)\n        );\n    }\n);\n\n// ************************************************************************* //\n",
+    "system/controlDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      controlDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolver          shockFluid;\n\nstartFrom       startTime;\n\nstartTime       0;\n\nstopAt          endTime;\n\nendTime         1.5;\n\ndeltaT         0.0002;\n\nwriteControl    adjustableRunTime;\n\nwriteInterval   0.15;\n\ncycleWrite      0;\n\nwriteFormat     binary;\n\nwritePrecision  6;\n\nwriteCompression off;\n\ntimeFormat      general;\n\ntimePrecision   6;\n\nrunTimeModifiable true;\n\nadjustTimeStep  yes;\n\nmaxCo           0.2;\n\nmaxDeltaT       0.05;\n\nfunctions\n{\n    extrema\n    {\n        type            volFieldValue;\n        operation       min;\n        libs            (\"libfieldFunctionObjects.so\");\n        fields          (rho p T);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n    mass\n    {\n        type            volFieldValue;\n        libs            (\"libfieldFunctionObjects.so\");\n        operation       volIntegrate;\n        fields          (rho rhoE);\n        writeControl    adjustableRunTime;\n        writeInterval   0.15;\n        writeFields     false;\n        cellZone        all;\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/decomposeParDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      decomposeParDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nnumberOfSubdomains 1;\n\nmethod          scotch;\n\n// ************************************************************************* //\n",
+    "system/fvSchemes": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSchemes;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nfluxScheme      Kurganov;\n\nddtSchemes\n{\n    default         Euler;\n}\n\ngradSchemes\n{\n    default         Gauss linear;\n}\n\ndivSchemes\n{\n    default         none;\n}\n\nlaplacianSchemes\n{\n    default         Gauss linear orthogonal;\n}\n\ninterpolationSchemes\n{\n    default         none;\n    reconstruct(rho) vanAlbada;\n    reconstruct(U)   vanAlbadaV;\n    reconstruct(T)   vanAlbada;\n    flux(rhoU)       linear;\n}\n\nsnGradSchemes\n{\n    default         orthogonal;\n}\n\n// ************************************************************************* //\n",
+    "system/fvSolution": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      fvSolution;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\nsolvers\n{\n    \"(rho|rhoU|rhoE).*\"\n    {\n        solver          diagonal;\n    }\n    \"U.*\"\n    {\n        solver          smoothSolver;\n        smoother        GaussSeidel;\n        nSweeps         2;\n        tolerance       1e-09;\n        relTol          0.01;\n    }\n    \"e.*\"\n    {\n        $U;\n        tolerance       1e-10;\n        relTol          0;\n    }\n}\n\nPIMPLE\n{\n    nOuterCorrectors 2;\n}\n\n// ************************************************************************* //\n",
+    "system/sample": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      sample;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ntype sets;\nlibs            (\"libsampling.so\");\ninterpolationScheme cellPoint;\nsetFormat       raw;\nsets\n{\n    horizontal\n    {\n        type lineFace; axis x; start (-4.995 0 0); end (4.995 0 0); nPoints 400;\n    }\n    vertical\n    {\n        type lineFace; axis y; start (0 -4.995 0); end (0 4.995 0); nPoints 400;\n    }\n}\nfields (rho U p T);\n\n// ************************************************************************* //\n",
+    "system/setFieldsDict": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      setFieldsDict;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ndefaultValues\n{\n    U       (0 0 0);\n    p       1.5;\n    T       1.40008419533;\n}\n\nzones\n{\n    southWest\n    {\n        type box; zoneType cell; box (-100 -100 -2) (0 0 2);\n        values { U (1.206 1.206 0); p 0.029; T 0.294220591773; }\n    }\n    southEast\n    {\n        type box; zoneType cell; box (0 -100 -2) (100 0 2);\n        values { U (0 1.206 0); p 0.3; T 0.789076195003; }\n    }\n    northWest\n    {\n        type box; zoneType cell; box (-100 0 -2) (0 100 2);\n        values { U (1.206 0 0); p 0.3; T 0.789076195003; }\n    }\n    northEast\n    {\n        type box; zoneType cell; box (0 0 -2) (100 100 2);\n        values { U (0 0 0); p 1.5; T 1.40008419533; }\n    }\n}\n\n// ************************************************************************* //\n",
+    "system/validateRiemann.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'positivity-and-conservation', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n",
+    "system/benchmarkParameters": "/*--------------------------------*- C++ -*----------------------------------*\\\n  =========                 |\n  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox\n   \\    /   O peration     | Website:  https://openfoam.org\n    \\  /    A nd           | Version:  13\n     \\/     M anipulation  |\n\\*---------------------------------------------------------------------------*/\nFoamFile\n{\n    format      ascii;\n    class       dictionary;\n    location    \"system\";\n    object      benchmarkParameters;\n}\n// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //\n\ngamma 1.4;\nR 0.714242760066;\nstudy restart_fidelity;\nmesh (600 600 1); maxCo 0.2; finalTime 1.5; splitTime 0.75;\nbranches continuous=(0,1.5); restart=(0,0.75)+(latestTime,1.5);\nmetrics (cellwiseRho cellwiseP cellwiseT cellwiseU centerline timeStepHistory extrema massDrift energyDrift outputAlignment);\n\n// ************************************************************************* //\n",
+    "Allrun": "#!/bin/sh\ncd \"${0%/*}\" || exit 1\n. \"$WM_PROJECT_DIR/bin/tools/RunFunctions\"\nset -eu\nmkdir -p continuous restart\ncp -r 0 constant system continuous/\ncp -r 0 constant system restart/\n(cd continuous && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\nsed -i 's/endTime         1.5/endTime         0.75/' restart/system/controlDict\n(cd restart && runApplication blockMesh && runApplication setFields && runApplication foamRun -solver shockFluid)\nsed -i 's/startFrom       startTime/startFrom       latestTime/; s/endTime         0.75/endTime         1.5/' restart/system/controlDict\n(cd restart && runApplication foamRun -solver shockFluid && runApplication -s sample foamPostProcess -latestTime -func sample)\npython3 system/compare_restart.py continuous restart\n",
+    "system/compare_restart.py": "#!/usr/bin/env python3\n\"\"\"Compare sampled Riemann branches and enforce finite positive states.\"\"\"\nfrom __future__ import annotations\nimport json, math, pathlib, re, sys, time\n\nNUMBER = re.compile(r\"[-+]?(?:\\d+(?:\\.\\d*)?|\\.\\d+)(?:[eE][-+]?\\d+)?\")\n\ndef latest_samples(root):\n    files = [p for p in root.rglob(\"*\") if p.is_file() and p.suffix in {\".raw\", \".xy\"}]\n    def key(path):\n        try: return float(path.parent.name)\n        except ValueError: return -1.0\n    latest = {}\n    for path in files:\n        name = path.name\n        if name not in latest or key(path) > key(latest[name]): latest[name] = path\n    rows = []\n    for path in sorted(latest.values()):\n        for line in path.read_text(errors=\"replace\").splitlines():\n            if not line.strip() or line.lstrip().startswith(\"#\"): continue\n            values = [float(x) for x in NUMBER.findall(line)]\n            # OF13 omits rho from sampled primitive fields; recover it from\n            # p=rho*R*T when the line has coordinate,Ux,Uy,Uz,p,T columns.\n            if len(values) >= 7:\n                rows.append(values[:7])\n            elif len(values) == 6 and values[5] > 0:\n                coordinate, ux, uy, uz, pressure, temperature = values\n                rows.append([coordinate, pressure/(8314.0/11640.3*temperature),\n                             ux, uy, uz, pressure, temperature])\n    return rows, [str(p) for p in sorted(latest.values())]\n\ndef branch_report(root):\n    rows, files = latest_samples(root)\n    finite = all(math.isfinite(x) for row in rows for x in row)\n    rho = [r[1] for r in rows]; p = [r[5] for r in rows]; temp = [r[6] for r in rows]\n    positive = bool(rows) and min(rho) > 0 and min(p) > 0 and min(temp) > 0\n    logs = \"\\n\".join(path.read_text(errors=\"replace\") for path in root.rglob(\"log.*\") if path.is_file())\n    steps = len(re.findall(r\"(?m)^Time =\", logs))\n    elapsed = [float(x) for x in re.findall(r\"ExecutionTime = ([0-9.eE+-]+)\", logs)]\n    return {\"root\": str(root), \"files\": files, \"rows\": rows, \"finite\": finite,\n            \"positive\": positive, \"minRho\": min(rho) if rho else None,\n            \"minP\": min(p) if p else None, \"minT\": min(temp) if temp else None,\n            \"maxRho\": max(rho) if rho else None, \"maxP\": max(p) if p else None,\n            \"steps\": steps, \"executionTime\": elapsed[-1] if elapsed else None}\n\ndef norms(reference, candidate, column):\n    n = min(len(reference), len(candidate))\n    if not n: return {\"L1\": None, \"L2\": None, \"LInf\": None, \"count\": 0}\n    delta = [abs(reference[i][column] - candidate[i][column]) for i in range(n)]\n    return {\"L1\": sum(delta)/n, \"L2\": math.sqrt(sum(x*x for x in delta)/n),\n            \"LInf\": max(delta), \"count\": n}\n\nroots = [pathlib.Path(arg) for arg in sys.argv[1:]] or [pathlib.Path(\"postProcessing\")]\nbranches = [branch_report(root) for root in roots]\ncomparisons = []\nif branches:\n    reference = branches[0][\"rows\"]\n    for branch in branches[1:]:\n        comparisons.append({\"candidate\": branch[\"root\"], \"rho\": norms(reference, branch[\"rows\"], 1),\n                            \"p\": norms(reference, branch[\"rows\"], 5),\n                            \"T\": norms(reference, branch[\"rows\"], 6)})\nfor branch in branches: branch.pop(\"rows\", None)\nstatus = \"pass\" if branches and all(b[\"finite\"] and b[\"positive\"] for b in branches) else \"fail\"\nreport = {\"study\": 'restart-fidelity', \"generatedAt\": time.time(), \"status\": status,\n          \"branches\": branches, \"comparisons\": comparisons}\npathlib.Path(\"riemann_diagnostics.json\").write_text(json.dumps(report, indent=2) + \"\\n\")\nprint(json.dumps(report, sort_keys=True))\nif status != \"pass\": raise SystemExit(1)\n"
+  }
+}
diff --git a/benchmarks/FoamBench_extended_openfoam13_measurement_specs.json b/benchmarks/FoamBench_extended_openfoam13_measurement_specs.json
new file mode 100644
index 0000000000000000000000000000000000000000..c06d298884d1b93b5a6833855d16514c1fb5ffde
--- /dev/null
+++ b/benchmarks/FoamBench_extended_openfoam13_measurement_specs.json
@@ -0,0 +1,4290 @@
+{
+  "schema_version": "easyfoam.extbench.measurement_specs.v1",
+  "status": "executable_measurement_contract",
+  "scope": "ExtBench only",
+  "reference_values_included": false,
+  "tolerances_included": false,
+  "prompt_policy": "case entry may be shown after usr_requirement; reference answers and thresholds are never included",
+  "operations": [
+    "boundary_difference",
+    "boundary_flux",
+    "boundary_flux_ratio",
+    "branchwise_wall_law",
+    "connected_phase_geometry",
+    "declared_line_sample",
+    "feature_detector",
+    "force_coefficient_table",
+    "volume_field_statistic",
+    "wall_resolution",
+    "window_field_statistic"
+  ],
+  "cases": {
+    "yPlusVerification/1": {
+      "case_id": "yPlusVerification/1",
+      "family": "yPlusVerification",
+      "variant": "1",
+      "branch_id": "wall_law_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/2": {
+      "case_id": "yPlusVerification/2",
+      "family": "yPlusVerification",
+      "variant": "2",
+      "branch_id": "wall_law_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/3": {
+      "case_id": "yPlusVerification/3",
+      "family": "yPlusVerification",
+      "variant": "3",
+      "branch_id": "low_re_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/4": {
+      "case_id": "yPlusVerification/4",
+      "family": "yPlusVerification",
+      "variant": "4",
+      "branch_id": "low_re_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/5": {
+      "case_id": "yPlusVerification/5",
+      "family": "yPlusVerification",
+      "variant": "5",
+      "branch_id": "low_re_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/6": {
+      "case_id": "yPlusVerification/6",
+      "family": "yPlusVerification",
+      "variant": "6",
+      "branch_id": "low_re_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/7": {
+      "case_id": "yPlusVerification/7",
+      "family": "yPlusVerification",
+      "variant": "7",
+      "branch_id": "low_re_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/8": {
+      "case_id": "yPlusVerification/8",
+      "family": "yPlusVerification",
+      "variant": "8",
+      "branch_id": "wall_law_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/9": {
+      "case_id": "yPlusVerification/9",
+      "family": "yPlusVerification",
+      "variant": "9",
+      "branch_id": "wall_law_profile",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "first_cell_yplus",
+          "definition": "wall-normal y+ of first cell center on the declared wall patch",
+          "measurement": {
+            "operation": "wall_resolution",
+            "quantity": "first_cell_yplus",
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "yPlusVerification/10": {
+      "case_id": "yPlusVerification/10",
+      "family": "yPlusVerification",
+      "variant": "10",
+      "branch_id": "multi_reynolds_branch",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "branchwise_wall_law_metrics",
+          "definition": "Spalding log-RMSE and first-cell yPlus preserved separately for Re_tau_180, Re_tau_395, and Re_tau_590 viscosity branches",
+          "measurement": {
+            "operation": "branchwise_wall_law",
+            "branches": [
+              "Re_tau_180",
+              "Re_tau_395",
+              "Re_tau_590"
+            ],
+            "time_semantics": "final_saved_time"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "risingBubble/1": {
+      "case_id": "risingBubble/1",
+      "family": "risingBubble",
+      "variant": "1",
+      "branch_id": "bubble_trajectory",
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+            "operation": "force_coefficient_table",
+            "column": "Cl",
+            "time_semantics": "declared_steady_window"
+          }
+        },
+        {
+          "metric": "Cm",
+          "definition": "moment coefficient about declared reference center and pitch axis",
+          "measurement": {
+            "operation": "force_coefficient_table",
+            "column": "Cm",
+            "time_semantics": "declared_steady_window"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "drivaerFastback/10": {
+      "case_id": "drivaerFastback/10",
+      "family": "drivaerFastback",
+      "variant": "10",
+      "branch_id": "transient_ddes",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "Cd_mean",
+          "definition": "time mean over statistically stationary DDES window",
+          "measurement": {
+            "operation": "force_coefficient_table",
+            "column": "Cd",
+            "statistic": "mean",
+            "time_semantics": "declared_stationary_window"
+          }
+        },
+        {
+          "metric": "Cd_rms",
+          "definition": "RMS fluctuation over the same window",
+          "measurement": {
+            "operation": "force_coefficient_table",
+            "column": "Cd",
+            "statistic": "rms",
+            "time_semantics": "declared_stationary_window"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/1": {
+      "case_id": "riemann2D/1",
+      "family": "riemann2D",
+      "variant": "1",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/2": {
+      "case_id": "riemann2D/2",
+      "family": "riemann2D",
+      "variant": "2",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/3": {
+      "case_id": "riemann2D/3",
+      "family": "riemann2D",
+      "variant": "3",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/4": {
+      "case_id": "riemann2D/4",
+      "family": "riemann2D",
+      "variant": "4",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/5": {
+      "case_id": "riemann2D/5",
+      "family": "riemann2D",
+      "variant": "5",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/6": {
+      "case_id": "riemann2D/6",
+      "family": "riemann2D",
+      "variant": "6",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/7": {
+      "case_id": "riemann2D/7",
+      "family": "riemann2D",
+      "variant": "7",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/8": {
+      "case_id": "riemann2D/8",
+      "family": "riemann2D",
+      "variant": "8",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/9": {
+      "case_id": "riemann2D/9",
+      "family": "riemann2D",
+      "variant": "9",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    },
+    "riemann2D/10": {
+      "case_id": "riemann2D/10",
+      "family": "riemann2D",
+      "variant": "10",
+      "branch_id": "profile_and_event_error",
+      "measurement_schema": "easyfoam.extbench.measurement.v1",
+      "principal_measurements": [
+        {
+          "metric": "centerline_profiles",
+          "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines",
+          "measurement": {
+            "operation": "declared_line_sample",
+            "fields": [
+              "rho",
+              "U",
+              "p",
+              "T"
+            ],
+            "time_semantics": "declared_final_or_aligned_time",
+            "profile_roles": [
+              "horizontal_centerline",
+              "vertical_centerline"
+            ]
+          }
+        },
+        {
+          "metric": "event_locations",
+          "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector",
+          "measurement": {
+            "operation": "feature_detector",
+            "input": "centerline_profiles",
+            "detector_version": "extbench.riemann.features.v1"
+          }
+        }
+      ],
+      "evidence_requirements": {
+        "retain": "original mesh plus all fields and numeric output times needed by time_semantics",
+        "provenance": [
+          "source field",
+          "mesh or patch/probe definition",
+          "dimensions and units",
+          "time semantics",
+          "method version"
+        ]
+      },
+      "proxies_forbidden": []
+    }
+  }
+}
diff --git a/benchmarks/FoamBench_extended_openfoam13_qoi_design.json b/benchmarks/FoamBench_extended_openfoam13_qoi_design.json
new file mode 100644
index 0000000000000000000000000000000000000000..ef9543f557a2d52b57b41d1f75a5994cc9aa09b9
--- /dev/null
+++ b/benchmarks/FoamBench_extended_openfoam13_qoi_design.json
@@ -0,0 +1,266 @@
+{
+  "schema_version": "foambench.qoi.design",
+  "status": "executable_reference_contract",
+  "frozen_reference_unchanged": true,
+  "scope": "Extended FoamBench scientific QoI contract",
+  "global_policy": {
+    "principal_qoi_is": "the declared physical response of the task, not a generic field extreme or output-availability fallback",
+    "acceptance_model": "Every principal response must satisfy its reference-anchored task-response contract and any declared reference-independent physical bounds. Both are reported explicitly and must pass jointly.",
+    "fallback_policy": "A fallback proxy may be reported as diagnostic or coverage evidence, but never silently replaces a principal QoI.",
+    "conditional_policy": "A conditional QoI is mandatory only when its declared applicability evidence is retained. Missing applicability evidence is reported as unavailable and never counted as a passed physical criterion.",
+    "branch_policy": "Cases are aggregated only with cases sharing the same response definition and branch. Variant relations are scored separately from absolute reference agreement.",
+    "time_policy": "Every history QoI declares endpoint, event, steady-window, or transient-trajectory semantics. Full-history means are not a default.",
+    "tolerance_policy": {
+      "global_default_percent": null,
+      "steady_scalar": "max(3*sigma_repeat, discretization_envelope, measurement_floor)",
+      "profile": "normalized L1/L2/Linf error with a declared reference norm and spatial window",
+      "event_location": "max(3*sigma_event, 2*local_cell_size, physical_measurement_floor)",
+      "trajectory": "time-aligned normalized RMSE plus event-time error",
+      "provisional_rule": "If repeatability and discretization evidence are unavailable, the result is provisional and cannot be called strict scientific validation."
+    },
+    "required_provenance": [
+      "source_fields_or_postprocessing_file",
+      "patch_region_or_probe_definition",
+      "unit_and_normalization",
+      "time_window_or_event_rule",
+      "method_version",
+      "reference_uncertainty_or_provisional_flag"
+    ]
+  },
+  "families": [
+    {
+      "family": "ERCOFTA_pump",
+      "scientific_question": "Does the rotating pump surrogate produce the intended pressure/flow response under speed, pressure, mesh, model, and transient branches?",
+      "branches": [
+        {
+          "id": "steady_pressure_flow",
+          "cases": ["1", "2", "3", "4", "6", "7", "8", "10"],
+          "principal_qois": [
+            {"name": "pressure_rise", "definition": "outlet-minus-inlet area-averaged static-pressure difference on the explicitly named patches", "source": "inlet/outlet patchAverage(p) outputs", "aggregation": "time-aligned saved history"},
+            {"name": "mass_flow_rate", "definition": "signed mass or volumetric flow from the explicitly named inlet flux, preserving phi dimensions", "source": "inlet face flux", "aggregation": "saved history; inlet/outlet conservation remains diagnostic until both fluxes are retained"}
+          ],
+          "diagnostics": ["shaft_torque", "shaft_power", "mass_balance_residual", "rotor_zone_extent"],
+          "relations": ["speed-response branch", "outlet-pressure branch", "mesh/rotor-zone sensitivity"]
+        },
+        {
+          "id": "transient_pressure_flow",
+          "cases": ["5", "9"],
+          "principal_qois": [
+            {"name": "pressure_rise_history", "definition": "time-aligned pressure-rise history between declared inlet/outlet patches", "aggregation": "trajectory over declared transient window"}
+          ],
+          "diagnostics": ["shaft_torque_history", "mass_balance_residual"]
+        }
+      ],
+      "forbidden_principal_proxies": ["domain_pressure_span", "global_p_min_max", "unweighted_internal_pressure_range"]
+    },
+    {
+      "family": "MRF_stirredReactor",
+      "scientific_question": "How do impeller rotation, rheology, baffles, mesh, and rotating formulation change mixer power and phase/interface response?",
+      "branches": [
+        {
+          "id": "single_phase_mixing",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9"],
+          "principal_qois": [
+            {"name": "volume_average_speed_final", "definition": "cell-volume-weighted final-time average velocity magnitude", "source": "retained U and cell volumes; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"}
+          ],
+          "diagnostics": ["stirrer_power_history", "volume_average_speed_history", "circulation", "mass_balance_residual"],
+          "relations": ["speed scaling", "mesh convergence", "baffle/model/sliding-mesh paired comparison"]
+        },
+        {
+          "id": "two_phase_interface",
+          "cases": ["10"],
+          "principal_qois": [
+            {"name": "volume_average_speed_history", "definition": "cell-volume-weighted domain average of velocity magnitude over the saved reference time window", "source": "U and cell volumes", "aggregation": "time-aligned trajectory"},
+            {"name": "volume_speed_rms_history", "definition": "cell-volume-weighted RMS spatial fluctuation of velocity magnitude about its instantaneous domain mean", "source": "U and cell volumes", "aggregation": "time-aligned trajectory"}
+          ],
+          "diagnostics": ["phase_volume_conservation", "interface_centroid", "phase_fraction_by_region"]
+        }
+      ],
+      "forbidden_principal_proxies": ["alpha_minimum_history", "global_alpha_minimum", "unrelated_phase_extreme"]
+    },
+    {
+      "family": "aerofoilNACA0012",
+      "scientific_question": "How do Mach number, angle of attack, turbulence model, mesh, and transient treatment change aerodynamic loads?",
+      "branches": [
+        {
+          "id": "aerodynamic_loads",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9", "10"],
+          "principal_qois": [
+            {"name": "Cd", "definition": "drag coefficient from the forceCoeffs header-addressed Cd column", "source": "declared aerofoil wall patches and drag direction", "aggregation": "steady-window mean, or transient mean plus RMS"},
+            {"name": "Cl", "definition": "lift coefficient from the header-addressed Cl column", "source": "declared wall patches and lift direction", "aggregation": "same window"},
+            {"name": "Cm", "definition": "moment coefficient about declared reference center and pitch axis", "source": "forceCoeffs output", "aggregation": "same window"}
+          ],
+          "diagnostics": ["surface_pressure_coefficient_profile", "separation_location", "residual_and_force_plateau"],
+          "relations": ["Mach response", "angle-of-attack load trend", "mesh convergence", "model comparison"]
+        }
+      ],
+      "extractor_requirements": ["parse forceCoeffs header by field name; never assume row index", "verify dragDir, liftDir, Aref, lRef, CofR", "do not compare a transient endpoint to a steady-window reference"]
+    },
+    {
+      "family": "compressibleBubbleCollapse",
+      "scientific_question": "How do pressure, bubble geometry, density ratio, wall distance, mesh, and compressibility change bubble-collapse dynamics?",
+      "branches": [
+        {
+          "id": "collapse_dynamics",
+          "cases": ["1", "3", "4", "5", "6", "7", "8", "9"],
+          "principal_qois": [
+            {"name": "equivalent_radius_final", "definition": "final radius from connected gas-phase volume, R=(3V/(4*pi))^(1/3) in 3D or the declared 2D area-equivalent convention", "source": "gas-phase alpha and cell volumes; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"},
+            {"name": "final_component_count", "definition": "number of retained connected gas components at the final saved field", "source": "gas-phase alpha and cell connectivity", "aggregation": "final saved field"}
+          ],
+          "diagnostics": ["bubble_centroid_history", "bubble_count", "interface_area", "minimum_pressure", "phase_volume_conservation"],
+          "relations": ["ambient-pressure trend", "wall-distance effect", "mesh/AMR convergence"]
+        },
+        {
+          "id": "materialized_single_bubble_response",
+          "cases": ["2"],
+          "principal_qois": [
+            {"name": "equivalent_radius_final", "definition": "final connected-gas equivalent radius for the single 50 um bubble actually materialized by setFieldsDict", "source": "gas-phase alpha and cell volumes; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"},
+            {"name": "final_component_count", "definition": "number of retained connected gas components at the final saved field", "source": "gas-phase alpha and cell connectivity", "aggregation": "final saved field"}
+          ],
+          "diagnostics": ["collapse_time_censored_diagnostic", "bubble_centroid_history", "phase_volume_conservation"],
+          "relations": []
+        },
+        {
+          "id": "axisymmetric_ring_interaction",
+          "cases": ["10"],
+          "principal_qois": [
+            {"name": "equivalent_radius_final", "definition": "final connected gas-region equivalent radius under the materialized axisymmetric wedge convention", "source": "gas-phase alpha and cell volumes with wedge volume factor; measurement-only C/Vc preparation is permitted", "aggregation": "component-preserving final field"},
+            {"name": "final_component_count", "definition": "number of retained connected gas components at the final saved field", "source": "gas-phase alpha and cell connectivity", "aggregation": "final saved field"}
+          ],
+          "diagnostics": ["component_count", "collapse_time_censored_diagnostic", "phase_volume_conservation"],
+          "relations": ["axisymmetric connected-region interaction"]
+        }
+      ],
+      "extractor_requirements": ["identify gas phase explicitly", "use connected components when multiple bubbles exist", "do not use global alpha minimum as a bubble-response substitute"]
+    },
+    {
+      "family": "drivaerFastback",
+      "scientific_question": "How do speed, mesh, wheel/ground treatment, turbulence model, and DDES treatment change vehicle aerodynamic loads?",
+      "branches": [
+        {
+          "id": "steady_aerodynamic_loads",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9"],
+          "principal_qois": [
+            {"name": "Cd", "definition": "header-addressed drag coefficient for body, wheels, and declared force patches", "source": "forceCoeffs", "aggregation": "last steady window"},
+            {"name": "Cl", "definition": "header-addressed lift coefficient", "source": "forceCoeffs", "aggregation": "last steady window"},
+            {"name": "Cm", "definition": "header-addressed moment coefficient about declared center", "source": "forceCoeffs", "aggregation": "last steady window"}
+          ],
+          "relations": ["speed scaling", "mesh convergence", "wheel/ground treatment comparison", "turbulence-model comparison"]
+        },
+        {
+          "id": "transient_ddes",
+          "cases": ["10"],
+          "principal_qois": [
+            {"name": "Cd_mean", "definition": "time mean over statistically stationary DDES window", "source": "forceCoeffs", "aggregation": "stationary-window mean"},
+            {"name": "Cd_rms", "definition": "RMS fluctuation over the same window", "source": "forceCoeffs", "aggregation": "stationary-window RMS"}
+          ],
+          "diagnostics": ["Cl_mean", "Cl_rms", "dominant_force_frequency", "stationarity_test"]
+        }
+      ],
+      "extractor_requirements": ["parse forceCoeffs headers and reference quantities", "do not compare DDES endpoint to steady reference", "report body/wheel patch coverage"]
+    },
+    {
+      "family": "nozzleCDV",
+      "scientific_question": "How do back pressure, mesh, discretisation, boundary specification, solver, turbulence, and dimension change nozzle flow structure and mass-flow response?",
+      "branches": [
+        {
+          "id": "shock_present",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9", "10"],
+          "principal_qois": [
+            {"name": "mass_flow_rate", "definition": "signed mass flux through the declared inlet section, preserving operating-point branches and the OpenFOAM phi sign", "source": "section face flux with phi dimensions [1 0 -1 0 0 0 0]", "aggregation": "final saved time per operating-point branch"}
+          ],
+          "conditional_qois": [
+            {"name": "shock_location", "condition": "a retained named centerline or versioned shock-detector output resolves one discontinuity", "definition": "location of maximum pressure-gradient or density-gradient on the declared centerline", "missing_evidence_status": "unavailable_not_passed"},
+            {"name": "pressure_ratio", "condition": "named inlet/outlet thermodynamic evidence and its static-or-total convention are retained", "definition": "declared static or total pressure ratio", "missing_evidence_status": "unavailable_not_passed"}
+          ],
+          "relations": ["back-pressure shock movement", "mesh convergence", "solver/discretisation comparison", "axisymmetric-vs-planar geometry"]
+        }
+      ],
+      "forbidden_principal_proxies": ["global_pressure_span", "pressure_min_max_without_section_or_centerline_definition"]
+    },
+    {
+      "family": "riemann2D",
+      "scientific_question": "How do numerical choices alter a four-quadrant compressible interaction while preserving the known/reference solution structure?",
+      "branches": [
+        {
+          "id": "profile_and_event_error",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9", "10"],
+          "principal_qois": [
+            {"name": "centerline_profiles", "definition": "named rho, p, T, and velocity profiles on fixed horizontal and vertical centerlines", "source": "named sample profiles", "aggregation": "declared final time or aligned time; L1 and Linf errors are computed by the comparison layer"},
+            {"name": "event_locations", "definition": "declared shock, contact, and rarefaction feature locations from the versioned feature detector", "source": "feature detector on centerline profiles", "aggregation": "same time; location error is computed by the comparison layer"}
+          ],
+          "diagnostics": ["rho_min", "p_min", "positivity_failures", "mass_momentum_energy_balance", "parallel_difference_norm"],
+          "relations": ["mesh convergence", "Courant sensitivity", "flux/limiter comparison", "domain-size sensitivity", "restart/decomposition invariance"]
+        }
+      ],
+      "extractor_requirements": ["the reference profile and variable columns must be explicit", "a sampled value or last column is never called error without candidate-reference subtraction", "feature detector and sampling coordinates are versioned"]
+    },
+    {
+      "family": "risingBubble",
+      "scientific_question": "How do mesh, interface treatment, density/viscosity, gravity, and solver choices change bubble rise and deformation?",
+      "branches": [
+        {
+          "id": "bubble_trajectory",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9", "10"],
+          "principal_qois": [
+            {"name": "bubble_centroid_y_final", "definition": "final volume-weighted centroid of the connected gas region from alpha threshold", "source": "gas-phase alpha and cell volumes; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"},
+            {"name": "equivalent_radius_final", "definition": "final connected gas-region equivalent radius", "source": "gas-phase alpha and cell volumes; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"},
+            {"name": "shape_aspect_ratio_final", "definition": "final principal-axis aspect ratio of the connected gas region", "source": "gas-phase alpha geometry and cell centres; measurement-only C/Vc preparation is permitted", "aggregation": "final saved field"}
+          ],
+          "diagnostics": ["bubble_centroid_y_history", "rise_velocity", "shape_aspect_ratio_history", "equivalent_diameter", "phase_volume_conservation", "interface_area", "breakup_or_coalescence_events"],
+          "relations": ["mesh convergence", "surface-tension/gravity branch", "density/viscosity branch", "solver/interface-scheme comparison"]
+        }
+      ],
+      "extractor_requirements": ["identify gas phase and connected component explicitly", "do not use global alpha minimum", "preserve transient histories rather than averaging all times into one scalar"]
+    },
+    {
+      "family": "supersonicCrossJet",
+      "scientific_question": "How do Mach number, jet/mainflow pressure ratio, injection angle, mesh, schemes, and solver formulation change jet penetration and shock structure?",
+      "branches": [
+        {
+          "id": "jet_trajectory_and_shock",
+          "cases": ["1", "2", "3", "4", "5", "6", "7", "8", "9", "10"],
+          "principal_qois": [
+            {"name": "jet_to_mainstream_mass_flux_ratio", "definition": "absolute ratio of the explicit phi mass flux through inlet2 to inlet1 at the final saved time", "source": "inlet1 and inlet2 patch fluxes; phi dimensions must be mass/time", "aggregation": "final saved time with branches kept separate"},
+            {"name": "interior_pressure_span", "definition": "max(p)-min(p) in the declared internal shock-search window -1<=x<=1 and 0.1<=y<=0.95", "source": "final retained p field and cell centres; uniform p fields are expanded over the retained cells", "aggregation": "final saved field; boundary cells outside the search window are excluded"}
+          ],
+          "diagnostics": ["jet_centerline_trajectory", "section_pressure_ratio", "shock_strength", "mass_balance_residual"],
+          "relations": ["Mach trend", "pressure-ratio trend", "injection-angle trend", "mesh/scheme/solver sensitivity"]
+        }
+      ],
+      "extractor_requirements": ["declare the jet-identifying field or momentum criterion", "declare section coordinates and interpolation", "do not use global pressure span as principal response"]
+    },
+    {
+      "family": "yPlusVerification",
+      "scientific_question": "Does the wall-normal velocity profile and first-cell wall resolution agree with the declared turbulent-wall-law or low-Reynolds-number verification target?",
+      "branches": [
+        {
+          "id": "wall_law_profile",
+          "cases": ["1", "2", "8", "9"],
+          "principal_qois": [
+            {"name": "first_cell_yplus", "definition": "wall-normal y+ of first cell center on the declared wall patch", "source": "wall distance and wall shear, or an explicitly named wall-normal profile with y+", "aggregation": "patch/profile endpoint"}
+          ],
+          "diagnostics": ["spalding_log_rmse", "achieved_Re_tau", "u_tau", "profile_residual_by_yplus_bin"],
+          "relations": ["mesh resolution", "turbulence-model comparison"]
+        },
+        {
+          "id": "low_re_profile",
+          "cases": ["3", "4", "5", "6", "7"],
+          "principal_qois": [
+            {"name": "first_cell_yplus", "definition": "first-cell wall resolution on the declared wall patch", "source": "wall distance and wall shear, or an explicitly named wall-normal profile with y+", "aggregation": "patch/profile endpoint"}
+          ],
+          "diagnostics": ["spalding_log_rmse", "achieved_Re_tau", "wall_shear_distribution", "boundedness"]
+        },
+        {
+          "id": "multi_reynolds_branch",
+          "cases": ["10"],
+          "principal_qois": [
+            {"name": "branchwise_wall_law_metrics", "definition": "Spalding log-RMSE and first-cell yPlus preserved separately for Re_tau_180, Re_tau_395, and Re_tau_590 viscosity branches", "source": "branch-labelled spalding_comparison.raw or explicitly named branch profiles", "aggregation": "no cross-branch averaging"}
+          ],
+          "diagnostics": ["branchwise_achieved_Re_tau", "branchwise_first_cell_yplus"]
+        }
+      ],
+      "extractor_requirements": ["use spalding_comparison.raw residual by name only as an intermediate evidence source", "recompute/verify u_tau, nu, y+, U+, and valid y+ range", "never let a U_z column or an all-zero placeholder define profile error"]
+    }
+  ]
+}
diff --git a/benchmarks/FoamBench_extended_openfoam13_reference_qois.json b/benchmarks/FoamBench_extended_openfoam13_reference_qois.json
new file mode 100644
index 0000000000000000000000000000000000000000..0826bb4cf1585be74a5f9fba44dde88198a96fa1
--- /dev/null
+++ b/benchmarks/FoamBench_extended_openfoam13_reference_qois.json
@@ -0,0 +1,304392 @@
+{
+  "case_count": 100,
+  "cases": {
+    "ERCOFTA_pump/1": {
+      "branch_id": "steady_pressure_flow",
+      "case_id": "ERCOFTA_pump/1",
+      "conditional_metrics": [],
+      "conditional_qois": {},
+      "conditional_status": {},
+      "diagnostic_qois": {},
+      "family": "ERCOFTA_pump",
+      "metric_roles": {
+        "mass_flow_rate": "principal",
+        "pressure_rise": "principal"
+      },
+      "principal_metrics": [
+        "pressure_rise",
+        "mass_flow_rate"
+      ],
+      "principal_qoi_group": "steady_pressure_flow",
+      "provenance": {
+        "case_dir": "anonymous-reference/extended/ERCOFTA_pump/1/case",
+        "evidence": {
+          "mass_flow_rate": [
+            "postProcessing/patchFlowRate(phi,patch=INLET)/0.000366/surfaceFieldValue.dat",
+            "postProcessing/patchFlowRate(phi,patch=INLET)/5e-07/surfaceFieldValue.dat"
+          ],
+          "pressure_rise": [
+            "postProcessing/patchAverage(p,patch=INLET)/0.000366/surfaceFieldValue.dat",
+            "postProcessing/patchAverage(p,patch=INLET)/0/surfaceFieldValue.dat",
+            "postProcessing/patchAverage(p,patch=OUTLET)/0.000366/surfaceFieldValue.dat",
+            "postProcessing/patchAverage(p,patch=OUTLET)/0/surfaceFieldValue.dat"
+          ]
+        },
+        "metric_methods": {
+          "mass_flow_rate": "explicit_mass_flux_history.v1",
+          "pressure_rise": "named_patch_pressure_history.v1"
+        }
+      },
+      "qois": {
+        "mass_flow_rate": {
+          "field_dimensions": "0 3 -1 0 0 0 0",
+          "kind": "time_history",
+          "points": [
+            {
+              "time": 5e-07,
+              "value": 0.09027
+            },
+            {
+              "time": 1e-06,
+              "value": 0.09027
+            },
+            {
+              "time": 1.5e-06,
+              "value": 0.09027
+            },
+            {
+              "time": 2e-06,
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+            {
+              "time": 2.5e-06,
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+            {
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+            {
+              "time": 3.5e-06,
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+            {
+              "time": 4e-06,
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+            {
+              "time": 4.5e-06,
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+            },
+            {
+              "time": 5e-06,
+              "value": 0.09027
+            },
+            {
+              "time": 5.5e-06,
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+            {
+              "time": 6e-06,
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+            {
+              "time": 6.5e-06,
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+              "time": 7e-06,
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+            {
+              "time": 7.5e-06,
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+            {
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+            {
+              "time": 8.5e-06,
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+            },
+            {
+              "time": 9e-06,
+              "value": 0.09027
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+            {
+              "time": 9.5e-06,
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+            {
+              "time": 1e-05,
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+    },
+    "yPlusVerification/9": {
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+      "case_id": "yPlusVerification/9",
+      "conditional_metrics": [],
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+      "principal_qoi_group": "wall_law_profile",
+      "provenance": {
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+        "evidence": {
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+            "postProcessing/sample/500/spalding_comparison.raw"
+          ]
+        },
+        "metric_methods": {
+          "first_cell_yplus": "spalding_named_profile_or_endpoint.v1"
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+          "relative_component": 0.1,
+          "threshold_source": "reference_anchored_repeatability_pending"
+        }
+      }
+    }
+  },
+  "design": "foambench.qoi.design",
+  "notes": [
+    "Principal reference bands test task-response agreement and are explicitly reference-anchored.",
+    "Definition-implied physical bounds are evaluated jointly when a sign or positivity rule is unambiguous.",
+    "Conditional QoIs remain unavailable rather than silently passing when their declared evidence is absent."
+  ],
+  "schema_version": "foambench.reference_qois",
+  "tolerance_status": "joint_physical_admissibility_and_reference_response_provisional"
+}
diff --git a/benchmarks/__init__.py b/benchmarks/__init__.py
new file mode 100644
index 0000000000000000000000000000000000000000..7d358702f21adf6849d7e18ba8458ff55d0d9990
--- /dev/null
+++ b/benchmarks/__init__.py
@@ -0,0 +1 @@
+"""FoamBench assets and evaluation utilities."""
diff --git a/benchmarks/assets/README.md b/benchmarks/assets/README.md
new file mode 100644
index 0000000000000000000000000000000000000000..61a1c3267a440caab0f1219976daf69ec837cfe3
--- /dev/null
+++ b/benchmarks/assets/README.md
@@ -0,0 +1,15 @@
+# ExtBench Geometry Assets
+
+These files are copied from the OpenFOAM 13 tutorial distribution used to
+build the benchmark reference cases. The OpenFOAM 13 distribution states in
+`README.org` and `COPYING` that the distributed files may be redistributed
+under the GNU General Public License, version 3 or later.
+
+The asset manifest records the original tutorial location and SHA-256 digest
+for every file. Materialization verifies the digest before copying an asset
+into a case. The assets are kept separate from the case JSON so the benchmark
+data remains readable and cases do not depend on a machine-specific `/opt`
+path.
+
+If a downstream distribution has additional provenance or licensing notices
+for the DrivAer geometry, add them here and to `manifest.json` before release.
diff --git a/benchmarks/assets/manifest.json b/benchmarks/assets/manifest.json
new file mode 100644
index 0000000000000000000000000000000000000000..da08ba71285bbdde74b189724a34d86141550643
--- /dev/null
+++ b/benchmarks/assets/manifest.json
@@ -0,0 +1,41 @@
+{
+  "schema_version": "foambench.asset-manifest.v1",
+  "license": "GPL-3.0-or-later (OpenFOAM 13 tutorial-derived files)",
+  "assets": {
+    "simpleRushtonMRF/stirrer4": {
+      "path": "benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer4.obj",
+      "sha256": "d64e176d6aa872857bb5b01791cc0441aa15ff8456440be7235f7481f658a117",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/simpleRushtonMRF/constant/geometry/stirrer4.obj"
+    },
+    "simpleRushtonMRF/stirrer6": {
+      "path": "benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer6.obj",
+      "sha256": "d0572aec19c41b2454ba0d7eecd1e07a7aae6aa98695f35ce781715e663ae40b",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/simpleRushtonMRF/constant/geometry/stirrer6.obj"
+    },
+    "simpleRushtonMRF/baffles": {
+      "path": "benchmarks/assets/openfoam13/simpleRushtonMRF/baffles.obj",
+      "sha256": "612cb86bfa2c842444ba86f203af31c712da3e807ed537013fefff8ab40f42a2",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/simpleRushtonMRF/constant/geometry/baffles.obj"
+    },
+    "naca0012/NACA0012": {
+      "path": "benchmarks/assets/openfoam13/naca0012/NACA0012.obj.gz",
+      "sha256": "9fd098e03da6178852d4f9837bc06d2f24599065644f951b481907513d835d90",
+      "source": "OpenFOAM-13/tutorials/resources/geometry/NACA0012.obj.gz"
+    },
+    "drivaerFastback/body": {
+      "path": "benchmarks/assets/openfoam13/drivaerFastback/body.obj.gz",
+      "sha256": "0622638e6d9e2ef61d739ef2ae699ce4d5fb212abeaaa6f4583da54f3da24efe",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/drivaerFastback/constant/geometry/body.obj.gz"
+    },
+    "drivaerFastback/frontWheels": {
+      "path": "benchmarks/assets/openfoam13/drivaerFastback/frontWheels.obj.gz",
+      "sha256": "f3e4f7f432c3e76d4f509fbba2429825acfc25ab696265df73f828504e6483b7",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/drivaerFastback/constant/geometry/frontWheels.obj.gz"
+    },
+    "drivaerFastback/rearWheels": {
+      "path": "benchmarks/assets/openfoam13/drivaerFastback/rearWheels.obj.gz",
+      "sha256": "02f25f876414a9a4cbdb9cfb08da9916ac49f7851d4658067abc371447f882ce",
+      "source": "OpenFOAM-13/tutorials/incompressibleFluid/drivaerFastback/constant/geometry/rearWheels.obj.gz"
+    }
+  }
+}
diff --git a/benchmarks/assets/openfoam13/drivaerFastback/body.obj.gz b/benchmarks/assets/openfoam13/drivaerFastback/body.obj.gz
new file mode 100644
index 0000000000000000000000000000000000000000..d1a3256c636ea2c0bd6b4e6c9d9c6ea34ca8f7cc
--- /dev/null
+++ b/benchmarks/assets/openfoam13/drivaerFastback/body.obj.gz
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:0622638e6d9e2ef61d739ef2ae699ce4d5fb212abeaaa6f4583da54f3da24efe
+size 2839115
diff --git a/benchmarks/assets/openfoam13/drivaerFastback/frontWheels.obj.gz b/benchmarks/assets/openfoam13/drivaerFastback/frontWheels.obj.gz
new file mode 100644
index 0000000000000000000000000000000000000000..c906943e5332eef633d50f071e0bbefb088d836b
--- /dev/null
+++ b/benchmarks/assets/openfoam13/drivaerFastback/frontWheels.obj.gz
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:f3e4f7f432c3e76d4f509fbba2429825acfc25ab696265df73f828504e6483b7
+size 860951
diff --git a/benchmarks/assets/openfoam13/drivaerFastback/rearWheels.obj.gz b/benchmarks/assets/openfoam13/drivaerFastback/rearWheels.obj.gz
new file mode 100644
index 0000000000000000000000000000000000000000..d3ee1ec4c8fea4e3b8bc048fc4dc3cbe9eccd733
--- /dev/null
+++ b/benchmarks/assets/openfoam13/drivaerFastback/rearWheels.obj.gz
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:02f25f876414a9a4cbdb9cfb08da9916ac49f7851d4658067abc371447f882ce
+size 940038
diff --git a/benchmarks/assets/openfoam13/naca0012/NACA0012.obj.gz b/benchmarks/assets/openfoam13/naca0012/NACA0012.obj.gz
new file mode 100644
index 0000000000000000000000000000000000000000..79fe8c9e0c2897f4dd0bb225ba9f1e256eaf3812
--- /dev/null
+++ b/benchmarks/assets/openfoam13/naca0012/NACA0012.obj.gz
@@ -0,0 +1,3 @@
+version https://git-lfs.github.com/spec/v1
+oid sha256:9fd098e03da6178852d4f9837bc06d2f24599065644f951b481907513d835d90
+size 112656
diff --git a/benchmarks/assets/openfoam13/simpleRushtonMRF/baffles.obj b/benchmarks/assets/openfoam13/simpleRushtonMRF/baffles.obj
new file mode 100644
index 0000000000000000000000000000000000000000..0316ee12a975bae5a809fb48bb882867dc2367e9
--- /dev/null
+++ b/benchmarks/assets/openfoam13/simpleRushtonMRF/baffles.obj
@@ -0,0 +1,38 @@
+# Wavefront OBJ file written 2024-10-12T17:20:59
+o baffles
+
+# points : 16
+# faces  : 8
+# zones  : 1
+#   0  patch0  (nFaces: 8)
+
+# <points count="16">
+v 0.353553 0.353553 0
+v 0.33234 0.33234 0
+v 0.353553 0.353553 1.2
+v 0.33234 0.33234 1.2
+v -0.33234 -0.33234 0
+v -0.353553 -0.353553 0
+v -0.33234 -0.33234 1.2
+v -0.353553 -0.353553 1.2
+v -0.353553 0.353553 0
+v -0.33234 0.33234 0
+v -0.353553 0.353553 1.2
+v -0.33234 0.33234 1.2
+v 0.33234 -0.33234 0
+v 0.353553 -0.353553 0
+v 0.33234 -0.33234 1.2
+v 0.353553 -0.353553 1.2
+# </points>
+
+# <faces count="8">
+g patch0
+f 2 4 3
+f 2 3 1
+f 6 8 7
+f 6 7 5
+f 10 12 11
+f 10 11 9
+f 14 16 15
+f 14 15 13
+# </faces>
diff --git a/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer4.obj b/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer4.obj
new file mode 100644
index 0000000000000000000000000000000000000000..1af963cd0e10835ddc0184cd6c9252276fad655c
--- /dev/null
+++ b/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer4.obj
@@ -0,0 +1,32 @@
+# Wavefront OBJ file
+# Regions:
+#     0    patch0
+#
+# points    : 16
+# triangles : 8
+#
+v -1.37773e-17 -0.075 0.57
+v -2.75546e-17 -0.15 0.57
+v -1.37773e-17 -0.075 0.63
+v -2.75546e-17 -0.15 0.63
+v -0.075 9.18485e-18 0.57
+v -0.15 1.83697e-17 0.57
+v -0.075 9.18485e-18 0.63
+v -0.15 1.83697e-17 0.63
+v 4.59243e-18 0.075 0.57
+v 9.18485e-18 0.15 0.57
+v 4.59243e-18 0.075 0.63
+v 9.18485e-18 0.15 0.63
+v 0.075 0 0.57
+v 0.15 0 0.57
+v 0.075 0 0.63
+v 0.15 0 0.63
+g patch0
+f 1 2 4
+f 1 4 3
+f 5 6 8
+f 5 8 7
+f 9 10 12
+f 9 12 11
+f 13 14 16
+f 13 16 15
diff --git a/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer6.obj b/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer6.obj
new file mode 100644
index 0000000000000000000000000000000000000000..765533665750649161ddaabc30265a4534e79d02
--- /dev/null
+++ b/benchmarks/assets/openfoam13/simpleRushtonMRF/stirrer6.obj
@@ -0,0 +1,47 @@
+# Wavefront OBJ file
+# Regions:
+#     0    zone0
+#     1    patch0
+#
+# points    : 24
+# triangles : 12
+#
+v 0.0375 -0.0649519 0.57
+v 0.075 -0.129904 0.57
+v 0.0375 -0.0649519 0.63
+v 0.075 -0.129904 0.63
+v -0.0375 -0.0649519 0.57
+v -0.075 -0.129904 0.57
+v -0.0375 -0.0649519 0.63
+v -0.075 -0.129904 0.63
+v -0.075 9.18485e-18 0.57
+v -0.15 1.83697e-17 0.57
+v -0.075 9.18485e-18 0.63
+v -0.15 1.83697e-17 0.63
+v -0.0375 0.0649519 0.57
+v -0.075 0.129904 0.57
+v -0.0375 0.0649519 0.63
+v -0.075 0.129904 0.63
+v 0.075 0 0.57
+v 0.15 0 0.57
+v 0.075 0 0.63
+v 0.15 0 0.63
+v 0.0375 0.0649519 0.57
+v 0.075 0.129904 0.57
+v 0.0375 0.0649519 0.63
+v 0.075 0.129904 0.63
+g zone0
+f 1 2 4
+f 1 4 3
+f 5 6 8
+f 5 8 7
+f 9 10 12
+f 9 12 11
+f 13 14 16
+f 13 16 15
+g patch0
+f 17 18 20
+f 17 20 19
+g zone0
+f 21 22 24
+f 21 24 23
diff --git a/benchmarks/evaluation/README.md b/benchmarks/evaluation/README.md
new file mode 100644
index 0000000000000000000000000000000000000000..36fdca68dd4dd9cb285dcb7b6d6ce2ba93b026a9
--- /dev/null
+++ b/benchmarks/evaluation/README.md
@@ -0,0 +1,12 @@
+# Standalone EasyFoam benchmark evaluator
+
+This directory contains the supplied evaluation implementation for Basic, Advanced and Extended tracks. See [Evaluation](../../docs/EVALUATION.md) for metric definitions, commands, dependencies, native-tool behavior and protocol boundaries, and the [dataset card](../../README.md) for contribution attribution.
+
+From the repository root:
+
+```bash
+python -m pip install -r requirements.txt
+python -m benchmarks.evaluation validate-profile --profile benchmarks/evaluation/profiles/extended.json
+```
+
+Agent campaign launchers and skill-evolution runtime code are distributed separately from this dataset. No model API key is needed to inspect the dataset or evaluate retained artifacts.
diff --git a/benchmarks/evaluation/__init__.py b/benchmarks/evaluation/__init__.py
new file mode 100644
index 0000000000000000000000000000000000000000..3357a7bf8ef6fba5ec1016f0fe08677c6b964132
--- /dev/null
+++ b/benchmarks/evaluation/__init__.py
@@ -0,0 +1,31 @@
+"""Dataset-independent FoamBench evaluation framework."""
+
+from pathlib import Path
+from typing import Any
+
+from .aggregate import aggregate_results
+from .models import BenchmarkProfile, CaseArtifact
+
+
+def evaluate_campaign(
+    profile: BenchmarkProfile,
+    *,
+    adapter_name: str,
+    run_root: Path,
+    output_dir: Path | None = None,
+    check_mesh: bool = False,
+    mesh_timeout: float = 120.0,
+) -> dict[str, Any]:
+    """Evaluate a campaign without importing the full pipeline at package import time."""
+    from .pipeline import evaluate_campaign as run_evaluation
+
+    return run_evaluation(
+        profile,
+        adapter_name=adapter_name,
+        run_root=run_root,
+        output_dir=output_dir,
+        check_mesh=check_mesh,
+        mesh_timeout=mesh_timeout,
+    )
+
+__all__ = ["BenchmarkProfile", "CaseArtifact", "aggregate_results", "evaluate_campaign"]
diff --git a/benchmarks/evaluation/__main__.py b/benchmarks/evaluation/__main__.py
new file mode 100644
index 0000000000000000000000000000000000000000..8f7704a5691aad1e269786d5dba9c3445d84de01
--- /dev/null
+++ b/benchmarks/evaluation/__main__.py
@@ -0,0 +1,10 @@
+import json
+import sys
+
+from .cli import main
+
+try:
+    raise SystemExit(main())
+except (OSError, ValueError, RuntimeError, json.JSONDecodeError) as exc:
+    print(f"foambench-evaluate: error: {exc}", file=sys.stderr)
+    raise SystemExit(2)
diff --git a/benchmarks/evaluation/adapters/__init__.py b/benchmarks/evaluation/adapters/__init__.py
new file mode 100644
index 0000000000000000000000000000000000000000..83885653cafb00f5cda617fd79049e0d6ea93962
--- /dev/null
+++ b/benchmarks/evaluation/adapters/__init__.py
@@ -0,0 +1,22 @@
+from .easyfoam import EasyFoamAdapter
+from .foamagent import FoamAgentAdapter
+from .chatcfd import ChatCFDAdapter
+from .coding_agent import CodingAgentAdapter
+
+ADAPTERS = {
+    "easyfoam": EasyFoamAdapter,
+    "foamagent": FoamAgentAdapter,
+    "chatcfd": ChatCFDAdapter,
+    "coding-agent": CodingAgentAdapter,
+}
+
+
+def create_adapter(name: str, *args, **kwargs):
+    try:
+        adapter = ADAPTERS[name]
+    except KeyError as exc:
+        raise ValueError(f"unknown evaluation adapter: {name}") from exc
+    return adapter(*args, **kwargs)
+
+
+__all__ = ["EasyFoamAdapter", "FoamAgentAdapter", "ChatCFDAdapter", "create_adapter"]
diff --git a/benchmarks/evaluation/adapters/chatcfd.py b/benchmarks/evaluation/adapters/chatcfd.py
new file mode 100644
index 0000000000000000000000000000000000000000..64d93a0b5b1f58a286d5ec2a80ff7f76a0b19d7a
--- /dev/null
+++ b/benchmarks/evaluation/adapters/chatcfd.py
@@ -0,0 +1,85 @@
+from __future__ import annotations
+
+from pathlib import Path
+
+from ..io import read_object
+from ..models import BenchmarkProfile, CaseArtifact
+from .common import duration, token_usage
+
+
+class ChatCFDAdapter:
+    """Normalize ChatCFD rollouts for the shared FoamBench scorer.
+
+    ChatCFD writes a case_run.log and keeps its model accounting in either a
+    rollout manifest or qa_logs.jsonl.  The adapter deliberately does not
+    infer case identity from generated files: a manifest is the reproducible
+    source of truth for benchmark membership.
+    """
+
+    def __init__(self, run_root: Path, profile: BenchmarkProfile):
+        self.run_root = run_root.resolve(strict=True)
+        self.profile = profile
+
+    def discover(self) -> dict[str, CaseArtifact]:
+        artifacts: dict[str, CaseArtifact] = {}
+        for manifest_path in sorted(self.run_root.rglob("rollout_manifest.json")):
+            manifest = read_object(manifest_path)
+            case_id = manifest.get("case_id")
+            if not isinstance(case_id, str) or case_id in artifacts:
+                continue
+            rollout = manifest_path.parent
+            case_ref = manifest.get("case_path", "case")
+            case_dir = Path(case_ref)
+            if not case_dir.is_absolute():
+                case_dir = rollout / case_dir
+            case_dir = case_dir.resolve()
+            family, variant = self.profile.identity(case_id)
+            logs = [p.resolve() for p in case_dir.glob("log.*") if p.is_file()]
+            logs.extend(p.resolve() for p in (case_dir / "case_run.log", case_dir / "Allrun.out", case_dir / "Allrun.err") if p.is_file())
+            normalized = dict(manifest)
+            normalized["duration_seconds"] = duration(manifest)
+            normalized["token_usage"] = token_usage(manifest)
+            if manifest.get("resource_measurement") == "request-journal-v1":
+                # Shared CSV reporting uses input/output names. Preserve the
+                # raw journal totals and completeness flags alongside aliases.
+                usage = normalized["token_usage"]
+                usage["input_tokens"] = usage["prompt_tokens"]
+                usage["output_tokens"] = usage["response_tokens"]
+            # Task selection and generation/repair have separate logs.
+            qa_logs = {p.resolve() for p in (rollout / "qa_logs.jsonl", case_dir / "qa_logs.jsonl") if p.is_file()}
+            if not normalized["token_usage"] and qa_logs:
+                totals = {"calls": 0, "prompt_tokens": 0, "response_tokens": 0, "reasoning_tokens": 0}
+                for path in sorted(qa_logs):
+                    for key, value in self._qa_usage(path).items():
+                        totals[key] += value
+                normalized["token_usage"] = totals
+            artifacts[case_id] = CaseArtifact(
+                case_id=case_id,
+                dataset=self.profile.dataset,
+                family=str(manifest.get("family") or family),
+                variant=str(manifest.get("variant") or variant),
+                replicate=int(manifest.get("replicate", 1)),
+                rollout_dir=rollout,
+                # Like Foam-Agent, ChatCFD supplies generic solver evidence,
+                # not an EasyFoam workflow workspace with formal run records.
+                workspace_dir=None,
+                case_dir=case_dir if case_dir.is_dir() else None,
+                manifest=normalized,
+                solver_logs=tuple(sorted(set(logs))),
+            )
+        return artifacts
+
+    @staticmethod
+    def _qa_usage(path: Path) -> dict[str, int]:
+        import json
+        totals = {"calls": 0, "prompt_tokens": 0, "response_tokens": 0, "reasoning_tokens": 0}
+        for line in path.read_text(encoding="utf-8").splitlines():
+            try:
+                row = json.loads(line)
+            except json.JSONDecodeError:
+                continue
+            totals["calls"] += 1
+            totals["prompt_tokens"] += int(row.get("prompt_tokens", 0) or 0)
+            totals["response_tokens"] += int(row.get("response_tokens", 0) or 0)
+            totals["reasoning_tokens"] += int(row.get("reasoning_tokens", 0) or 0)
+        return totals
diff --git a/benchmarks/evaluation/adapters/coding_agent.py b/benchmarks/evaluation/adapters/coding_agent.py
new file mode 100644
index 0000000000000000000000000000000000000000..86cd546edd83130c3a93c4741e3e81537714a4a2
--- /dev/null
+++ b/benchmarks/evaluation/adapters/coding_agent.py
@@ -0,0 +1,48 @@
+from __future__ import annotations
+
+from pathlib import Path
+
+from ..io import read_object
+from ..models import BenchmarkProfile, CaseArtifact
+
+
+class CodingAgentAdapter:
+    """Use externally recorded output discovery; impose no agent-side file contract."""
+
+    def __init__(self, run_root: Path, profile: BenchmarkProfile):
+        self.run_root = run_root.resolve(strict=True)
+        self.profile = profile
+
+    def discover(self) -> dict[str, CaseArtifact]:
+        result = {}
+        for path in sorted(self.run_root.glob("*/*/replicate_001/rollout_manifest.json")):
+            manifest = read_object(path)
+            if manifest.get("experiment_kind") != "requirement_only_coding_agent.v1":
+                raise ValueError(f"Unexpected experiment manifest: {path}")
+            case_id = manifest["case_id"]
+            if case_id in result:
+                raise ValueError(f"Duplicate case: {case_id}")
+            rollout = path.parent
+            workspace = rollout / "workspace"
+            ref = manifest.get("output_discovery", {}).get("case_ref")
+            case_dir = None
+            if isinstance(ref, str):
+                candidate = (workspace / ref).resolve()
+                if not candidate.is_relative_to(workspace.resolve()):
+                    raise ValueError(f"Case escapes workspace: {ref}")
+                case_dir = candidate
+            logs = []
+            for ref in manifest.get("solver_log_refs", []):
+                candidate = (rollout / ref).resolve()
+                if not candidate.is_relative_to(rollout.resolve()):
+                    raise ValueError(f"Log escapes rollout: {ref}")
+                if candidate.is_file():
+                    logs.append(candidate)
+            family, variant = self.profile.identity(case_id)
+            result[case_id] = CaseArtifact(
+                case_id=case_id, dataset=self.profile.dataset, family=family, variant=variant,
+                replicate=1, rollout_dir=rollout, workspace_dir=workspace, case_dir=case_dir,
+                manifest={**manifest, "agent_mode": "coding-only", "domain_assets_enabled": False},
+                solver_logs=tuple(logs),
+            )
+        return result
diff --git a/benchmarks/evaluation/adapters/common.py b/benchmarks/evaluation/adapters/common.py
new file mode 100644
index 0000000000000000000000000000000000000000..1025a23ab47daf7bfc3f1834b2ff02ae7b1d3a05
--- /dev/null
+++ b/benchmarks/evaluation/adapters/common.py
@@ -0,0 +1,71 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from ..io import read_object
+
+
+def formal_records(workspace: Path) -> tuple[Path, ...]:
+    paths: list[Path] = []
+    workflow_path = workspace / "workflow.json"
+    if workflow_path.is_file():
+        workflow = read_object(workflow_path)
+        refs = workflow.get("artifacts", {}).get("run_records", [])
+        for ref in refs if isinstance(refs, list) else []:
+            if isinstance(ref, str):
+                paths.append(workspace / ref)
+    paths.extend(workspace.glob("runs/formal-*/run_record.json"))
+    unique = {path.resolve() for path in paths if path.is_file()}
+    return tuple(sorted(unique))
+
+
+def successful_formal_records(paths: tuple[Path, ...]) -> tuple[Path, ...]:
+    successful = []
+    for path in paths:
+        record = read_object(path)
+        if record.get("mode") == "formal" and record.get("terminal_status") == "succeeded":
+            successful.append(path)
+    return tuple(successful)
+
+
+def logs_from_records(workspace: Path, records: tuple[Path, ...]) -> tuple[Path, ...]:
+    logs: list[Path] = []
+    for path in records:
+        record = read_object(path)
+        for command in record.get("commands", []) if isinstance(record.get("commands"), list) else []:
+            if not isinstance(command, dict):
+                continue
+            for key in ("stdout_ref", "stderr_ref"):
+                ref = command.get(key)
+                if isinstance(ref, str):
+                    candidate = workspace / ref
+                    if candidate.is_file():
+                        logs.append(candidate.resolve())
+    return tuple(dict.fromkeys(logs))
+
+
+def token_usage(manifest: dict[str, Any]) -> dict[str, Any]:
+    usage = manifest.get("token_usage")
+    if isinstance(usage, dict):
+        return dict(usage)
+    attempts = manifest.get("attempts")
+    if isinstance(attempts, list) and attempts and isinstance(attempts[-1], dict):
+        usage = attempts[-1].get("token_usage")
+    return dict(usage) if isinstance(usage, dict) else {}
+
+
+def duration(manifest: dict[str, Any]) -> float | None:
+    value = manifest.get("duration_seconds")
+    if isinstance(value, (int, float)):
+        return float(value)
+    process = manifest.get("process")
+    if isinstance(process, dict) and isinstance(process.get("duration_seconds"), (int, float)):
+        return float(process["duration_seconds"])
+    attempts = manifest.get("attempts")
+    values = [
+        float(item["duration_seconds"])
+        for item in attempts if isinstance(attempts, list) and isinstance(item, dict)
+        and isinstance(item.get("duration_seconds"), (int, float))
+    ] if isinstance(attempts, list) else []
+    return sum(values) if values else None
diff --git a/benchmarks/evaluation/adapters/easyfoam.py b/benchmarks/evaluation/adapters/easyfoam.py
new file mode 100644
index 0000000000000000000000000000000000000000..f6e833ef7bdd10e7fefaa7bd8275e8f588d04c6f
--- /dev/null
+++ b/benchmarks/evaluation/adapters/easyfoam.py
@@ -0,0 +1,108 @@
+from __future__ import annotations
+
+from pathlib import Path
+
+from ..foam import FATAL_RE, final_log_time, normal_end
+from ..foam_io import read_text
+from ..io import read_object
+from ..models import BenchmarkProfile, CaseArtifact
+from .common import duration, formal_records, logs_from_records, successful_formal_records, token_usage
+
+
+class EasyFoamAdapter:
+    """Normalize supported EasyFoam rollout layouts."""
+
+    def __init__(self, run_root: Path, profile: BenchmarkProfile):
+        self.run_root = run_root.resolve(strict=True)
+        self.profile = profile
+
+    def discover(self) -> dict[str, CaseArtifact]:
+        artifacts: dict[str, CaseArtifact] = {}
+        legacy = sorted(self.run_root.glob("*/*/replicate_*/rollout_manifest.json"))
+        current = sorted(self.run_root.rglob("run_manifest.json")) if not legacy else []
+        for path in [*legacy, *current]:
+            manifest = read_object(path)
+            case_id = manifest.get("case_id")
+            if not isinstance(case_id, str) or case_id in artifacts:
+                continue
+            rollout = path.parent
+            workspace = self._workspace(rollout, manifest)
+            family, variant = self.profile.identity(case_id)
+            coding_only = manifest.get("agent_mode") == "coding-only" or manifest.get("domain_assets_enabled") is False
+            case_dir = workspace / "case" if workspace else None
+            if coding_only and case_dir and case_dir.is_dir():
+                # Coding-only rollouts intentionally do not retain EasyFoam
+                # formal records. Avoid scanning their large workspaces for
+                # workflow/run-record artifacts before using generic logs.
+                records = ()
+                generic_logs = [item for item in case_dir.glob("log.*") if item.is_file()]
+                generic_logs.extend(
+                    item for item in (case_dir / "Allrun.out", case_dir / "Allrun.err") if item.is_file()
+                )
+                logs = _successful_generic_logs(generic_logs)
+            else:
+                records = formal_records(workspace) if workspace and workspace.is_dir() else ()
+                logs = logs_from_records(workspace, successful_formal_records(records)) if workspace else ()
+            normalized = dict(manifest)
+            normalized["duration_seconds"] = duration(manifest)
+            normalized["token_usage"] = token_usage(manifest)
+            artifacts[case_id] = CaseArtifact(
+                case_id=case_id,
+                dataset=self.profile.dataset,
+                family=str(manifest.get("family") or family),
+                variant=str(manifest.get("variant") or variant),
+                replicate=int(manifest.get("replicate", 1)),
+                rollout_dir=rollout,
+                workspace_dir=workspace,
+                case_dir=case_dir,
+                manifest=normalized,
+                formal_run_records=records,
+                solver_logs=logs,
+                workflow_path=workspace / "workflow.json" if workspace else None,
+                evidence_summary_path=workspace / "evidence_summary.json" if workspace else None,
+            )
+        return artifacts
+
+    def _workspace(self, rollout: Path, manifest: dict) -> Path | None:
+        direct = rollout / "workspace"
+        if direct.is_dir():
+            return direct.resolve()
+        ref = manifest.get("workspace_ref")
+        if isinstance(ref, str):
+            candidate = Path(ref)
+            if not candidate.is_absolute():
+                candidate = self.run_root / candidate
+            return candidate.resolve()
+        return None
+
+
+def _successful_generic_logs(paths: list[Path]) -> tuple[Path, ...]:
+    """Select final successful solver evidence without failed repair/postprocess logs."""
+    canonical_paths = tuple(sorted({item.resolve() for item in paths if item.name == "log.foamRun"}))
+    if canonical_paths:
+        # log.foamRun is the runner's canonical solver log.  Do not read
+        # multi-hundred-MB repair logs during artifact discovery; execution
+        # and numerical gates perform the substantive log checks later.
+        return canonical_paths
+    if paths:
+        # Avoid eagerly loading every repair/post-processing log merely to
+        # choose evidence. Prefer the newest generic log; gate parsing will
+        # validate its contents when it is actually evaluated.
+        existing = [item.resolve() for item in paths if item.is_file()]
+        if existing:
+            return (max(existing, key=lambda item: item.stat().st_mtime),)
+    evidence = []
+    for path in sorted({item.resolve() for item in paths}):
+        text = read_text(path)
+        if FATAL_RE.search(text):
+            continue
+        evidence.append((path, text, final_log_time(text)))
+    canonical = [item for item in evidence if item[0].name == "log.foamRun"]
+    if canonical:
+        return tuple(item[0] for item in canonical)
+    timed = [item for item in evidence if item[2] is not None]
+    if timed:
+        latest = max(float(item[2]) for item in timed if item[2] is not None)
+        return tuple(item[0] for item in timed if item[2] == latest)
+    ended = [item for item in evidence if normal_end(item[1])]
+    return tuple(item[0] for item in (ended or evidence))
diff --git a/benchmarks/evaluation/adapters/foamagent.py b/benchmarks/evaluation/adapters/foamagent.py
new file mode 100644
index 0000000000000000000000000000000000000000..3b184bd1e91e101cb21cbb54017d792d27211048
--- /dev/null
+++ b/benchmarks/evaluation/adapters/foamagent.py
@@ -0,0 +1,57 @@
+from __future__ import annotations
+
+from pathlib import Path
+
+from ..io import read_object
+from ..models import BenchmarkProfile, CaseArtifact
+from .common import duration, token_usage
+
+
+class FoamAgentAdapter:
+    def __init__(self, run_root: Path, profile: BenchmarkProfile):
+        self.run_root = run_root.resolve(strict=True)
+        self.profile = profile
+
+    def discover(self) -> dict[str, CaseArtifact]:
+        artifacts: dict[str, CaseArtifact] = {}
+        for path in sorted(self.run_root.glob("*/*/replicate_*/rollout_manifest.json")):
+            manifest = read_object(path)
+            case_id = manifest.get("case_id")
+            if not isinstance(case_id, str) or case_id in artifacts:
+                continue
+            rollout = path.parent
+            case_dir = rollout / "case"
+            family, variant = self.profile.identity(case_id)
+            logs = [item for item in case_dir.glob("log.*") if item.is_file()]
+            logs.extend(item for item in (case_dir / "Allrun.out", case_dir / "Allrun.err") if item.is_file())
+            process = manifest.get("process") if isinstance(manifest.get("process"), dict) else {}
+            attempts = manifest.get("attempts") if isinstance(manifest.get("attempts"), list) else []
+            last_attempt = attempts[-1] if attempts and isinstance(attempts[-1], dict) else {}
+            normalized = dict(manifest)
+            normalized["return_code"] = process.get(
+                "return_code", last_attempt.get("return_code", manifest.get("return_code"))
+            )
+            normalized["timed_out"] = bool(process.get(
+                "timed_out", last_attempt.get("timed_out", manifest.get("timed_out", False))
+            ))
+            normalized["duration_seconds"] = duration(manifest)
+            normalized["token_usage"] = token_usage(manifest)
+            for metrics_path in (rollout / "llm_metrics.json", rollout / "attempt_001.llm_metrics.json"):
+                if metrics_path.is_file():
+                    normalized["token_usage"] = token_usage({"token_usage": read_object(metrics_path)})
+                    break
+            if isinstance(manifest.get("execution"), dict):
+                normalized["source_execution"] = manifest["execution"]
+            artifacts[case_id] = CaseArtifact(
+                case_id=case_id,
+                dataset=self.profile.dataset,
+                family=str(manifest.get("family") or family),
+                variant=str(manifest.get("variant") or variant),
+                replicate=int(manifest.get("replicate", 1)),
+                rollout_dir=rollout,
+                workspace_dir=None,
+                case_dir=case_dir,
+                manifest=normalized,
+                solver_logs=tuple(sorted({item.resolve() for item in logs})),
+            )
+        return artifacts
diff --git a/benchmarks/evaluation/aggregate.py b/benchmarks/evaluation/aggregate.py
new file mode 100644
index 0000000000000000000000000000000000000000..b452dfad838c15c9b261add0402d581e09b6623a
--- /dev/null
+++ b/benchmarks/evaluation/aggregate.py
@@ -0,0 +1,100 @@
+from __future__ import annotations
+
+import statistics
+from collections import Counter
+from typing import Any
+
+
+def _rate(count: int, denominator: int) -> float | None:
+    return count / denominator if denominator else None
+
+
+def aggregate_results(rows: list[dict[str, Any]]) -> dict[str, Any]:
+    total = len(rows)
+    execution = sum(bool(row.get("scores", {}).get("execution_pass")) for row in rows)
+    numerical = sum(bool(row.get("scores", {}).get("numerical_pass")) for row in rows)
+    qoi = sum(
+        bool(
+            row.get("scores", {}).get(
+                "physics_grounded_qoi_pass",
+                row.get("scores", {}).get("qoi_pass"),
+            )
+        )
+        for row in rows
+    )
+    end_to_end = sum(bool(row.get("scores", {}).get("end_to_end_pass")) for row in rows)
+    ratios = [float(row.get("qoi", {}).get("effective_pass_ratio", 0.0)) for row in rows]
+    coverage = [
+        float(comparison["qoi_coverage_fraction"])
+        for row in rows
+        for comparison in [row.get("qoi", {}).get("comparison")]
+        if isinstance(comparison, dict) and isinstance(comparison.get("qoi_coverage_fraction"), (int, float))
+    ]
+    failures = Counter(
+        failure
+        for row in rows
+        for failure in row.get("failure_categories", [])
+    )
+    return {
+        "task_count": total,
+        "execution_pass_count": execution,
+        "execution_pass_rate": _rate(execution, total),
+        "numerical_pass_count": numerical,
+        "numerical_pass_rate_all_tasks": _rate(numerical, total),
+        "numerical_pass_rate_execution_pass": _rate(numerical, execution),
+        "physics_grounded_qoi_pass_count": qoi,
+        "physics_grounded_qoi_pass_rate_all_tasks": _rate(qoi, total),
+        "physics_grounded_qoi_pass_rate_execution_pass": _rate(qoi, execution),
+        "end_to_end_pass_count": end_to_end,
+        "end_to_end_pass_rate": _rate(end_to_end, total),
+        "mean_qoi_pass_ratio_all_tasks": statistics.fmean(ratios) if ratios else None,
+        "mean_qoi_coverage_evaluated": statistics.fmean(coverage) if coverage else None,
+        "failure_taxonomy": dict(sorted(failures.items())),
+    }
+
+
+def aggregate_evolution(groups: dict[str, list[dict[str, Any]]]) -> dict[str, Any]:
+    """Paired repeated-split reporting. Duplicate tasks remain group-qualified."""
+    metrics = ("execution_pass", "numerical_pass", "physics_grounded_qoi_pass", "end_to_end_pass")
+
+    def summarize(rows):
+        for row in rows:
+            for side in ("initial", "evolved"):
+                scores = row.get("reporting_scores", {}).get(side)
+                if not isinstance(scores, dict) or any(type(scores.get(key)) is not bool for key in metrics):
+                    raise ValueError("independent reporting scores are missing; reward is not a pass metric")
+                if scores["end_to_end_pass"] != all(scores[key] for key in metrics[:3]):
+                    raise ValueError("TAR is inconsistent with the three task-level checks")
+        return {metric: {
+            side: {"count": sum(row["reporting_scores"][side][metric] for row in rows),
+                   "rate": statistics.fmean(row["reporting_scores"][side][metric] for row in rows)}
+            for side in ("initial", "evolved")
+        } | {
+            "gain": statistics.fmean(int(row["reporting_scores"]["evolved"][metric]) - int(row["reporting_scores"]["initial"][metric]) for row in rows),
+            "failed_to_passed": sum(not row["reporting_scores"]["initial"][metric] and row["reporting_scores"]["evolved"][metric] for row in rows),
+            "passed_to_failed": sum(row["reporting_scores"]["initial"][metric] and not row["reporting_scores"]["evolved"][metric] for row in rows),
+        } for metric in metrics}
+
+    per_group = {}
+    all_rows = []
+    for group_id, rows in groups.items():
+        keys = {(row["dataset"], row["case_id"]) for row in rows}
+        if not rows or len(keys) != len(rows):
+            raise ValueError(f"empty or duplicate test tasks in group {group_id}")
+        per_group[group_id] = {"task_count": len(rows), "metrics": summarize(rows)}
+        all_rows.extend(dict(row, group_id=group_id) for row in rows)
+    families = {family: summarize([row for row in all_rows if row["family"] == family])
+                for family in sorted({row["family"] for row in all_rows})}
+    means = {metric: {side: {
+        "mean": statistics.fmean(group["metrics"][metric][side]["rate"] for group in per_group.values()),
+        "min": min(group["metrics"][metric][side]["rate"] for group in per_group.values()),
+        "max": max(group["metrics"][metric][side]["rate"] for group in per_group.values()),
+    } for side in ("initial", "evolved")} for metric in metrics}
+    return {"groups": per_group, "group_rates": means, "families": families,
+            "family_equal_weight_rates": {metric: {side: statistics.fmean(family[metric][side]["rate"] for family in families.values())
+                                                  for side in ("initial", "evolved")} for metric in metrics},
+            "test_records_per_condition": len(all_rows),
+            "unique_task_count": len({(row["dataset"], row["case_id"]) for row in all_rows}),
+            "test_frequency": dict(Counter(f"{row['dataset']}::{row['case_id']}" for row in all_rows)),
+            "interpretation": "Descriptive repeated splits; overlapping tasks and groups are not independent samples.",
+            "cases": all_rows}
diff --git a/benchmarks/evaluation/basic_advanced.py b/benchmarks/evaluation/basic_advanced.py
new file mode 100644
index 0000000000000000000000000000000000000000..0586cfa67db837b406e31e74d13fb59bca469d10
--- /dev/null
+++ b/benchmarks/evaluation/basic_advanced.py
@@ -0,0 +1,807 @@
+#!/usr/bin/env python3
+"""Structured QoIs shared by FoamBench Basic and Advanced references/candidates."""
+from __future__ import annotations
+
+import argparse
+import json
+import math
+import re
+import subprocess
+from pathlib import Path
+from typing import Any, Callable
+
+from .foam_arrays import FoamArrayError, foam_path, read_scalar_field, read_vector_field
+from .foam_io import magnitude, read_text
+from .io import utc_now, write_json
+from .schema import validate
+
+
+ADVANCED_TEMPLATE = {
+    "Cavity_LES": "Cavity", "Cavity_SA": "Cavity", "Cavity_geometry_1": "Cavity",
+    "Cylinder_LES": "Cylinder", "Cylinder_SA": "Cylinder",
+    "Diamond_Obstacle_KOMEGASST": "Obstacle", "Diamond_Obstacle_SA": "Obstacle",
+    "Double_Square_SA": "Obstacle", "Rectangular_Obstacle_KOMEGASST": "Obstacle",
+    "Rectangular_Obstacle_SA": "Obstacle", "counterFlowFlame2D_KE": "counterFlowFlame2D",
+    "counterFlowFlame2D_SA": "counterFlowFlame2D", "nozzleFlow2D_SA": "Nozzle",
+    "obliqueShock_KE": "Shock", "obliqueShock_LES": "Shock", "wedge_SA": "Shock",
+}
+
+GROUPS = {
+    "BernardCells": "thermal_state", "Cavity": "cavity_response", "Cylinder": "wake_response",
+    "counterFlowFlame2D": "flame_response", "damBreakWithObstacle": "free_surface_response",
+    "forwardStep": "shock_response", "obliqueShock": "shock_response", "wedge": "shock_response",
+    "Shock": "shock_response", "pitzDaily": "separation_response", "Obstacle": "obstacle_response",
+    "shallowWaterWithSquareBump": "surface_response", "squareBend": "bend_response",
+    "Nozzle": "nozzle_response",
+}
+
+PHYSICS_METRICS = {
+    "BernardCells": ("temperature_min", "temperature_max", "convection_mean_speed"),
+    "Cavity": ("response_speed_max", "reverse_flow_min_u"),
+    "Cylinder": ("wake_deficit_final",),
+    "counterFlowFlame2D": ("species_sum_max_error", "reaction_temperature_span"),
+    "damBreakWithObstacle": ("water_volume_relative_drift", "front_net_advance"),
+    "forwardStep": ("supersonic_volume_fraction", "shock_pressure_jump_ratio"),
+    "obliqueShock": ("supersonic_volume_fraction", "shock_pressure_jump_ratio"),
+    "wedge": ("supersonic_volume_fraction", "shock_pressure_jump_ratio"),
+    "Shock": ("supersonic_volume_fraction", "shock_pressure_jump_ratio"),
+    "pitzDaily": ("reverse_flow_volume_fraction", "streamwise_pressure_change_magnitude"),
+    "Obstacle": ("streamwise_pressure_change_magnitude",),
+    "shallowWaterWithSquareBump": ("mid_bump_height_relative_change",),
+    "squareBend": ("streamwise_pressure_change_magnitude",),
+    "Nozzle": ("flow_speed_max",),
+}
+
+# Each family already extracts one spatial response profile.  Making that
+# profile mandatory adds field-structure discrimination without introducing
+# another observable or extractor.  Scalar envelopes remain the
+# reference-independent admissibility check; profiles are the deliberately
+# stricter, reference-anchored response-shape check.
+PRINCIPAL_RESPONSE_PROFILES = {
+    "BernardCells": ("thermal_vertical_profile",),
+    "Cavity": ("centerline_velocity_profiles",),
+    "Cylinder": ("wake_velocity_profiles",),
+    "counterFlowFlame2D": ("reaction_zone_profile",),
+    "damBreakWithObstacle": ("free_surface_profile",),
+    "forwardStep": ("pressure_mach_profiles",),
+    "obliqueShock": ("pressure_mach_profiles",),
+    "wedge": ("pressure_mach_profiles",),
+    "Shock": ("pressure_mach_profiles",),
+    "pitzDaily": ("separation_profiles",),
+    "Obstacle": ("separation_profiles",),
+    "shallowWaterWithSquareBump": ("surface_profile",),
+    "squareBend": ("bend_axial_profile",),
+    "Nozzle": ("nozzle_axial_profile",),
+}
+
+
+def principal_metrics(template: str) -> tuple[str, ...]:
+    return PHYSICS_METRICS[template] + PRINCIPAL_RESPONSE_PROFILES[template]
+
+
+def numeric_times(case: Path) -> list[tuple[float, Path]]:
+    result = []
+    for child in case.iterdir():
+        if child.is_dir():
+            try:
+                result.append((float(child.name), child))
+            except ValueError:
+                pass
+    return sorted(result)
+
+
+def align(values: list[Any], count: int) -> list[Any]:
+    if len(values) == count:
+        return values
+    if len(values) == 1 and count:
+        return values * count
+    return []
+
+
+def scalars(directory: Path, name: str, count: int) -> list[float]:
+    path = foam_path(directory, name)
+    if path is None:
+        return []
+    try:
+        return align(read_scalar_field(path), count)
+    except (FoamArrayError, OSError, ValueError):
+        return []
+
+
+def vectors(directory: Path, name: str, count: int) -> list[tuple[float, float, float]]:
+    path = foam_path(directory, name)
+    if path is None:
+        return []
+    try:
+        return align(read_vector_field(path), count)
+    except (FoamArrayError, OSError, ValueError):
+        match = re.search(
+            r"internalField\s+uniform\s+\(([-+0-9.eE]+)\s+([-+0-9.eE]+)\s+([-+0-9.eE]+)\)",
+            read_text(path),
+        )
+        return [(float(match[1]), float(match[2]), float(match[3]))] * count if match else []
+
+
+def geometry(case: Path) -> tuple[list[tuple[float, float, float]], list[float], float, Path]:
+    times = numeric_times(case)
+    for time, directory in reversed(times):
+        c_path, v_path = foam_path(directory, "C"), foam_path(directory, "Vc")
+        if c_path and v_path:
+            centres = read_vector_field(c_path)
+            volumes = align(read_scalar_field(v_path), len(centres))
+            if centres and volumes:
+                return centres, volumes, time, directory
+    # C and Vc are measurement products, not required solver outputs. The
+    # independent evaluator also runs without prepare_campaign(), so recover
+    # the same geometric quantities directly from a retained static polyMesh.
+    # This uses no reference values and never writes into the frozen case.
+    if not times:
+        raise ValueError(f"no retained time directories for measurement: {case}")
+    from .retained_fields import derive_cell_geometry
+    try:
+        volumes, centres, _ = derive_cell_geometry(case)
+    except (ValueError, OSError) as exc:
+        raise ValueError(f"missing C/Vc and retained mesh geometry unavailable: {case}: {exc}") from exc
+    time, directory = times[-1]
+    count = raw_field_count(directory)
+    if count is not None and count != len(centres):
+        raise ValueError(f"retained field/mesh cell count mismatch: {case}")
+    return centres, volumes, time, directory
+
+
+def raw_field_count(directory: Path) -> int | None:
+    for name, reader in (("alpha.water", read_scalar_field), ("h", read_scalar_field),
+                         ("T", read_scalar_field), ("p", read_scalar_field), ("U", read_vector_field)):
+        path = foam_path(directory, name)
+        if path is None:
+            continue
+        try:
+            count = len(reader(path))
+        except (FoamArrayError, OSError, ValueError):
+            continue
+        if count > 1:
+            return count
+    return None
+
+
+def geometry_for_time(
+    case: Path, directory: Path, fallback_centres: list[tuple[float, float, float]], fallback_volumes: list[float],
+) -> tuple[list[tuple[float, float, float]], list[float]]:
+    expected = raw_field_count(directory)
+    if expected in {None, len(fallback_centres)}:
+        return fallback_centres, fallback_volumes
+    c_path, v_path = foam_path(directory, "C"), foam_path(directory, "Vc")
+    if not c_path or not v_path:
+        for function in ("writeCellCentres", "writeCellVolumes"):
+            completed = subprocess.run(
+                ["foamPostProcess", "-case", str(case), "-func", function, "-time", directory.name],
+                stdout=subprocess.DEVNULL, stderr=subprocess.STDOUT, check=False,
+            )
+            if completed.returncode != 0:
+                raise ValueError(f"{case}: {function} failed at time {directory.name}")
+        c_path, v_path = foam_path(directory, "C"), foam_path(directory, "Vc")
+    if not c_path or not v_path:
+        raise ValueError(f"{case}: no time-local C/Vc at {directory.name}")
+    centres = read_vector_field(c_path)
+    volumes = align(read_scalar_field(v_path), len(centres))
+    if len(centres) != expected or not volumes:
+        raise ValueError(f"{case}: time-local geometry mismatch at {directory.name}")
+    return centres, volumes
+
+
+def bounds(centres: list[tuple[float, float, float]]) -> tuple[list[float], list[float]]:
+    return ([min(p[i] for p in centres) for i in range(3)], [max(p[i] for p in centres) for i in range(3)])
+
+
+def primary_axis(spans: list[float]) -> int:
+    """Choose x/y/z deterministically when extents differ only by roundoff."""
+    largest = max(spans)
+    return next(i for i, span in enumerate(spans) if math.isclose(span, largest, rel_tol=1e-12, abs_tol=0.0))
+
+
+def weighted(values: list[float], volumes: list[float]) -> float:
+    denominator = sum(volumes)
+    return sum(value * volume for value, volume in zip(values, volumes)) / denominator
+
+
+def bins(
+    centres: list[tuple[float, float, float]], volumes: list[float], axis: int,
+    fields: dict[str, list[float]], *, count: int = 41,
+    selector: Callable[[tuple[float, float, float]], bool] | None = None,
+) -> list[list[float]]:
+    low, high = bounds(centres)
+    span = high[axis] - low[axis]
+    groups: list[list[int]] = [[] for _ in range(count)]
+    for index, point in enumerate(centres):
+        if selector is not None and not selector(point):
+            continue
+        slot = min(count - 1, max(0, int((point[axis] - low[axis]) / max(span, 1e-30) * count)))
+        groups[slot].append(index)
+    rows = []
+    for indices in groups:
+        if not indices:
+            continue
+        weights = [volumes[i] for i in indices]
+        row = [weighted([centres[i][axis] for i in indices], weights)]
+        for values in fields.values():
+            row.append(weighted([values[i] for i in indices], weights))
+        rows.append(row)
+    return rows
+
+
+def profile(profile_id: str, coordinate: str, rows: list[list[float]], fields: list[str]) -> dict[str, Any]:
+    return {"profile_id": profile_id, "columns": [coordinate, *fields], "rows": rows}
+
+
+def named_profiles(items: list[dict[str, Any]]) -> dict[str, Any]:
+    return {"kind": "named_profiles", "profiles": items}
+
+
+def history(points: list[dict[str, float]]) -> dict[str, Any]:
+    return {"kind": "time_history", "points": points}
+
+
+def velocity_fields(directory: Path, count: int) -> tuple[list[tuple[float, float, float]], dict[str, list[float]]]:
+    velocity = vectors(directory, "U", count)
+    if not velocity:
+        return [], {}
+    return velocity, {
+        "u": [v[0] for v in velocity], "v": [v[1] for v in velocity],
+        "speed": magnitude(velocity),
+    }
+
+
+def thermo(case: Path) -> tuple[float, float]:
+    text = read_text(case / "constant" / "physicalProperties")
+    mw = re.search(r"(?m)^\s*molWeight\s+([-+0-9.eE]+)\s*;", text)
+    cp = re.search(r"(?m)^\s*Cp\s+([-+0-9.eE]+)\s*;", text)
+    if not mw or not cp:
+        return 1.4, 287.0
+    gas = 8314.46261815324 / float(mw[1])
+    heat = float(cp[1])
+    return (heat / (heat - gas) if heat > gas else 1.4), gas
+
+
+def state_fields(case: Path, directory: Path, count: int) -> dict[str, list[float]]:
+    _, fields = velocity_fields(directory, count)
+    for name in (
+        "p", "p_rgh", "rho", "T", "CH4", "O2", "CO2", "H2O", "N2", "Qdot",
+        "alpha.water", "alpha.fuel", "h",
+    ):
+        values = scalars(directory, name, count)
+        if values:
+            fields[name] = values
+    if fields.get("T") and fields.get("speed"):
+        gamma, gas = thermo(case)
+        fields["Mach"] = [u / math.sqrt(gamma * gas * t) if t > 0 else 0.0 for u, t in zip(fields["speed"], fields["T"])]
+    hu = vectors(directory, "hU", count)
+    if hu and fields.get("h"):
+        fields["Froude"] = [
+            q / h / math.sqrt(9.81 * h) if h > 1e-12 else 0.0
+            for q, h in zip(magnitude(hu), fields["h"])
+        ]
+    return fields
+
+
+def line_profile(
+    profile_id: str, centres: list[tuple[float, float, float]], volumes: list[float],
+    axis: int, fixed_axis: int, fraction: float, fields: dict[str, list[float]], names: list[str],
+) -> dict[str, Any]:
+    low, high = bounds(centres)
+    target = low[fixed_axis] + fraction * (high[fixed_axis] - low[fixed_axis])
+    target = min((point[fixed_axis] for point in centres), key=lambda value: abs(value - target))
+    bandwidth = max((high[fixed_axis] - low[fixed_axis]) / 41.0, 1e-12)
+    selected = lambda point: abs(point[fixed_axis] - target) <= bandwidth
+    usable = {name: fields[name] for name in names if name in fields}
+    return profile(profile_id, "xyz"[axis], bins(centres, volumes, axis, usable, selector=selected), list(usable))
+
+
+def section_profile(
+    profile_id: str, centres: list[tuple[float, float, float]], volumes: list[float], axis: int,
+    fields: dict[str, list[float]], names: list[str],
+) -> dict[str, Any]:
+    usable = {name: fields[name] for name in names if name in fields}
+    return profile(profile_id, "xyz"[axis], bins(centres, volumes, axis, usable), list(usable))
+
+
+def histories(
+    case: Path, centres: list[tuple[float, float, float]], volumes: list[float],
+    measure: Callable[[dict[str, list[float]], list[tuple[float, float, float]], list[float]], float | None],
+) -> dict[str, Any]:
+    points = []
+    for time, directory in numeric_times(case):
+        local_centres, local_volumes = geometry_for_time(case, directory, centres, volumes)
+        fields = state_fields(case, directory, len(local_centres))
+        value = measure(fields, local_centres, local_volumes)
+        if value is not None and math.isfinite(value):
+            points.append({"time": time, "value": float(value)})
+    return history(points)
+
+
+def shock_events(value: dict[str, Any]) -> dict[str, Any]:
+    events = []
+    for item in value.get("profiles", []):
+        columns, rows = item["columns"], item["rows"]
+        if "p" not in columns or len(rows) < 2:
+            continue
+        p_index = columns.index("p")
+        candidates = []
+        coordinate_min, coordinate_max = rows[0][0], rows[-1][0]
+        interior_low = coordinate_min + 0.05 * (coordinate_max - coordinate_min)
+        interior_high = coordinate_max - 0.05 * (coordinate_max - coordinate_min)
+        for left, right in zip(rows, rows[1:]):
+            dx = right[0] - left[0]
+            coordinate = 0.5 * (right[0] + left[0])
+            if dx > 0 and interior_low < coordinate < interior_high:
+                candidates.append((abs(right[p_index] - left[p_index]) / dx, coordinate, dx))
+        if candidates:
+            _, coordinate, cell = max(candidates)
+            events.append({"profile_id": item["profile_id"], "field": "p", "coordinate": coordinate, "local_cell_size": cell})
+    return {"kind": "profile_feature_locations", "events": events}
+
+
+def relative_drift(values: list[float]) -> float | None:
+    finite_values = [float(value) for value in values if math.isfinite(value)]
+    if len(finite_values) < 2:
+        return None
+    scale = max(abs(finite_values[0]), sum(abs(value) for value in finite_values) / len(finite_values), 1e-12)
+    return (max(finite_values) - min(finite_values)) / scale
+
+
+def pressure_change(
+    pressure: list[float], centres: list[tuple[float, float, float]], volumes: list[float], axis: int,
+) -> float | None:
+    if not pressure:
+        return None
+    cut = max(1, len(pressure) // 10)
+    ordered = sorted(zip(centres, pressure, volumes), key=lambda item: item[0][axis])
+    first, last = ordered[:cut], ordered[-cut:]
+    return weighted([p for _, p, _ in first], [w for _, _, w in first]) - weighted(
+        [p for _, p, _ in last], [w for _, _, w in last]
+    )
+
+
+def inventory_series(case: Path, field_name: str) -> list[float]:
+    centres, volumes, _, _ = geometry(case)
+    values = []
+    for _, directory in numeric_times(case):
+        local_centres, local_volumes = geometry_for_time(case, directory, centres, volumes)
+        field = scalars(directory, field_name, len(local_centres))
+        if field:
+            values.append(sum(value * volume for value, volume in zip(field, local_volumes)))
+    return values
+
+
+def shock_pressure_jump_ratio(profiles: dict[str, Any]) -> float | None:
+    ratios = []
+    for item in profiles.get("profiles", []):
+        columns, rows = item.get("columns", []), item.get("rows", [])
+        if "p" not in columns:
+            continue
+        index = columns.index("p")
+        for left, right in zip(rows, rows[1:]):
+            low, high = sorted((float(left[index]), float(right[index])))
+            if low > 0:
+                ratios.append(high / low)
+    return max(ratios) if ratios else None
+
+
+def family_qois(case: Path, template: str) -> dict[str, Any]:
+    centres, volumes, _, latest = geometry(case)
+    low, high = bounds(centres)
+    spans = [high[i] - low[i] for i in range(3)]
+    primary = primary_axis(spans)
+    secondary = 1 if primary == 0 else 0
+    fields = state_fields(case, latest, len(centres))
+    if fields.get("p"):
+        pressure_mean = weighted(fields["p"], volumes)
+        fields["p_gauge"] = [value - pressure_mean for value in fields["p"]]
+    qois: dict[str, Any] = {}
+
+    def downstream_min_u(f: dict[str, list[float]], c: list[tuple[float, float, float]], v: list[float]) -> float | None:
+        values = [u for point, u in zip(c, f.get("u", [])) if point[primary] >= low[primary] + 0.5 * spans[primary]]
+        return min(values) if values else None
+
+    def middle_section_mean(name: str, fraction: float = 0.5) -> Callable[[dict[str, list[float]], list[tuple[float, float, float]], list[float]], float | None]:
+        def measure(f: dict[str, list[float]], c: list[tuple[float, float, float]], v: list[float]) -> float | None:
+            values = f.get(name, [])
+            if not values:
+                return None
+            local_low, local_high = bounds(c)
+            target = local_low[primary] + fraction * (local_high[primary] - local_low[primary])
+            target = min((point[primary] for point in c), key=lambda value: abs(value - target))
+            width = max((local_high[primary] - local_low[primary]) / 41.0, 1e-12)
+            selected = [(value, volume) for point, value, volume in zip(c, values, v) if abs(point[primary] - target) <= width]
+            return weighted([item[0] for item in selected], [item[1] for item in selected]) if selected else None
+        return measure
+
+    def wake_deficit(f: dict[str, list[float]], c: list[tuple[float, float, float]], v: list[float]) -> float | None:
+        streamwise = f.get("u", [])
+        if not streamwise:
+            return None
+        local_low, local_high = bounds(c)
+        span = local_high[primary] - local_low[primary]
+        width = max(span / 41.0, 1e-12)
+        section_values = []
+        for fraction in (0.10, 0.65):
+            target = local_low[primary] + fraction * span
+            target = min((point[primary] for point in c), key=lambda value: abs(value - target))
+            selected = [(u, volume) for point, u, volume in zip(c, streamwise, v)
+                        if abs(point[primary] - target) <= width]
+            if not selected:
+                return None
+            section_values.append(weighted([item[0] for item in selected], [item[1] for item in selected]))
+        upstream, wake = section_values
+        return (upstream - wake) / max(abs(upstream), 1e-12)
+
+    if template == "BernardCells":
+        qois["thermal_vertical_profile"] = named_profiles([
+            line_profile("vertical_centerline", centres, volumes, 1, 0, 0.5, fields, ["T", "u", "v", "speed"])
+        ])
+        qois["circulation_strength_history"] = histories(case, centres, volumes, lambda f, c, v: weighted(f["speed"], v) if f.get("speed") else None)
+        if fields.get("T"):
+            qois["temperature_min"] = min(fields["T"])
+            qois["temperature_max"] = max(fields["T"])
+        if fields.get("speed"):
+            qois["convection_mean_speed"] = weighted(fields["speed"], volumes)
+    elif template == "Cavity":
+        qois["centerline_velocity_profiles"] = named_profiles([
+            line_profile("vertical_centerline", centres, volumes, 1, 0, 0.5, fields, ["u", "v", "speed"]),
+            line_profile("horizontal_centerline", centres, volumes, 0, 1, 0.5, fields, ["u", "v", "speed"]),
+        ])
+        qois["kinetic_energy_history"] = histories(case, centres, volumes, lambda f, c, w: 0.5 * weighted([v*v for v in f["speed"]], w) if f.get("speed") else None)
+        if fields.get("speed"):
+            qois["response_speed_max"] = max(fields["speed"])
+        if fields.get("u"):
+            qois["reverse_flow_min_u"] = min(fields["u"])
+    elif template == "Cylinder":
+        qois["wake_velocity_profiles"] = named_profiles([
+            line_profile(f"wake_x_{fraction:.2f}", centres, volumes, secondary, primary, fraction, fields, ["u", "v", "speed", "p_gauge"])
+            for fraction in (0.65, 0.80)
+        ])
+        qois["wake_deficit_history"] = histories(case, centres, volumes, wake_deficit)
+        points = qois["wake_deficit_history"].get("points", [])
+        if points:
+            qois["wake_deficit_final"] = float(points[-1]["value"])
+    elif template == "counterFlowFlame2D":
+        names = ["T", "CO2"] + (["Qdot"] if fields.get("Qdot") else [])
+        qois["reaction_zone_profile"] = named_profiles([section_profile("reaction_axis", centres, volumes, primary, fields, names)])
+        if fields.get("Qdot"):
+            qois["heat_release_history"] = histories(case, centres, volumes, lambda f, c, w: sum(v*vol for v, vol in zip(f["Qdot"], w)) if f.get("Qdot") else None)
+        else:
+            qois["peak_temperature_history"] = histories(case, centres, volumes, lambda f, c, v: max(f["T"]) if f.get("T") else None)
+        species = [fields[name] for name in ("CH4", "O2", "CO2", "H2O", "N2") if fields.get(name)]
+        if len(species) == 5:
+            qois["species_sum_max_error"] = max(abs(sum(values) - 1.0) for values in zip(*species))
+        if fields.get("T"):
+            qois["reaction_temperature_span"] = max(fields["T"]) - min(fields["T"])
+    elif template == "damBreakWithObstacle":
+        qois["front_position_history"] = histories(case, centres, volumes, lambda f, c, v: max((p[0] for p, a in zip(c, f.get("alpha.water", [])) if a >= 0.5), default=None))
+        alpha = fields.get("alpha.water", [])
+        rows = []
+        for slot in bins(centres, volumes, 0, {"alpha": alpha}):
+            x = slot[0]
+            width = spans[0] / 41
+            wet_y = [p[1] for p, a in zip(centres, alpha) if abs(p[0] - x) <= width and a >= 0.5]
+            if wet_y:
+                rows.append([x, max(wet_y)])
+        qois["free_surface_profile"] = named_profiles([profile("alpha_0.5_surface", "x", rows, ["surface_y"])])
+        drift = relative_drift(inventory_series(case, "alpha.water"))
+        if drift is not None:
+            qois["water_volume_relative_drift"] = drift
+        front_points = qois["front_position_history"].get("points", [])
+        if len(front_points) >= 2:
+            qois["front_net_advance"] = float(front_points[-1]["value"]) - float(front_points[0]["value"])
+    elif template in {"forwardStep", "obliqueShock", "wedge", "Shock"}:
+        profiles = named_profiles([
+            line_profile(f"streamline_{fraction:.2f}", centres, volumes, primary, secondary, fraction, fields, ["p", "Mach", "u", "speed"])
+            for fraction in (0.25, 0.50, 0.75)
+        ])
+        qois["pressure_mach_profiles"] = profiles
+        qois["shock_feature_locations"] = shock_events(profiles)
+        if fields.get("Mach"):
+            qois["supersonic_volume_fraction"] = sum(
+                volume for mach, volume in zip(fields["Mach"], volumes) if mach > 1.0
+            ) / sum(volumes)
+        jump = shock_pressure_jump_ratio(profiles)
+        if jump is not None:
+            qois["shock_pressure_jump_ratio"] = jump
+    elif template in {"pitzDaily", "Obstacle"}:
+        qois["separation_profiles"] = named_profiles([
+            section_profile("streamwise_sections", centres, volumes, primary, fields, ["u", "v", "speed", "p_gauge"]),
+            *[line_profile(f"wake_{fraction:.2f}", centres, volumes, secondary, primary, fraction, fields, ["u", "v", "speed", "p_gauge"]) for fraction in (0.65, 0.80)],
+        ])
+        qois["recirculation_strength_history"] = histories(case, centres, volumes, downstream_min_u)
+        downstream = [
+            (u, volume) for point, u, volume in zip(centres, fields.get("u", []), volumes)
+            if point[primary] >= low[primary] + 0.5 * spans[primary]
+        ]
+        if downstream:
+            qois["reverse_flow_volume_fraction"] = sum(
+                volume for u, volume in downstream if u < 0.0
+            ) / sum(volume for _, volume in downstream)
+        change = pressure_change(fields.get("p", []) or fields.get("p_rgh", []), centres, volumes, primary)
+        if change is not None:
+            qois["streamwise_pressure_change_magnitude"] = abs(change)
+    elif template == "shallowWaterWithSquareBump":
+        qois["surface_profile"] = named_profiles([section_profile("bump_axis", centres, volumes, primary, fields, ["h", "Froude"])])
+        qois["mid_bump_height_history"] = histories(case, centres, volumes, middle_section_mean("h"))
+        height_points = qois["mid_bump_height_history"].get("points", [])
+        if len(height_points) >= 2:
+            first, last = float(height_points[0]["value"]), float(height_points[-1]["value"])
+            qois["mid_bump_height_relative_change"] = abs(last - first) / max(abs(first), 1e-12)
+    elif template in {"squareBend", "Nozzle"}:
+        prefix = "bend" if template == "squareBend" else "nozzle"
+        qois[f"{prefix}_axial_profile"] = named_profiles([section_profile("axial_sections", centres, volumes, primary, fields, ["p", "p_rgh", "Mach", "u", "speed"])])
+        def pressure_drop(f: dict[str, list[float]], c: list[tuple[float, float, float]], v: list[float]) -> float | None:
+            return pressure_change(f.get("p") or f.get("p_rgh") or [], c, v, primary)
+        qois["pressure_drop_history"] = histories(case, centres, volumes, pressure_drop)
+        if template == "squareBend":
+            change = pressure_change(fields.get("p", []) or fields.get("p_rgh", []), centres, volumes, primary)
+            if change is not None:
+                qois["streamwise_pressure_change_magnitude"] = abs(change)
+        else:
+            drift = relative_drift(inventory_series(case, "alpha.fuel"))
+            if drift is not None:
+                qois["transported_phase_inventory_relative_drift"] = drift
+            if fields.get("speed"):
+                qois["flow_speed_max"] = max(fields["speed"])
+    else:
+        raise ValueError(f"no structured QoI family for {template}")
+    return qois
+
+
+def structured_errors(name: str, value: Any) -> list[str]:
+    if isinstance(value, (int, float)) and not isinstance(value, bool):
+        return [] if math.isfinite(float(value)) else [f"{name}: non-finite scalar"]
+    if not isinstance(value, dict):
+        return [f"{name}: not structured"]
+    if value.get("kind") == "time_history":
+        return [] if len(value.get("points", [])) >= 2 else [f"{name}: fewer than two history points"]
+    if value.get("kind") == "named_profiles":
+        profiles = value.get("profiles", [])
+        return [] if profiles and all(len(p.get("rows", [])) >= 2 and len(p.get("columns", [])) >= 2 for p in profiles) else [f"{name}: incomplete profiles"]
+    if value.get("kind") == "profile_feature_locations":
+        return [] if value.get("events") else [f"{name}: no feature events"]
+    return [f"{name}: unsupported kind"]
+
+
+def extract(
+    case: Path,
+    case_id: str,
+    requested_metrics: list[str] | None = None,
+    *,
+    required_metrics: list[str] | None = None,
+    log_paths: list[Path] | None = None,
+) -> dict[str, Any]:
+    family = case_id.split("/", 1)[0]
+    template = ADVANCED_TEMPLATE.get(case_id, family)
+    values = family_qois(case, template)
+    requested = requested_metrics or sorted(values)
+    required = required_metrics or requested
+    selected = {name: values[name] for name in requested if name in values}
+    missing = sorted(set(required) - set(selected))
+    errors = [
+        error for name, value in selected.items() if name in required
+        for error in structured_errors(name, value)
+    ]
+    _, _, latest_time, _ = geometry(case)
+    complete = not missing and not errors
+    return {
+        "schema_version": "foambench.qoi.candidate", "case_id": case_id, "family": template,
+        "latest_time": latest_time, "status": "complete" if complete else "incomplete",
+        "principal_qoi_group": GROUPS[template],
+        "principal_metrics": sorted(name for name in required if name in selected),
+        "required_metrics": required, "missing_metrics": missing, "qois": selected,
+        "health": {"status": "pass" if complete else "fail", "checks": {
+            "principal_qoi_complete": not missing, "structured_qoi_valid": not errors,
+            "measurement_geometry_available": True, "no_proxy_fallback": True,
+        }, "validation_errors": errors},
+    }
+
+
+FIELD_NORMALIZATION_FLOORS = {
+    "p": 1.0, "p_gauge": 1.0, "p_rgh": 1.0, "T": 0.1, "CO2": 1e-6, "Qdot": 1e-3,
+    "u": 1e-5, "v": 1e-5, "speed": 1e-5, "Mach": 1e-4,
+    "h": 1e-6, "Froude": 1e-4, "surface_y": 1e-6,
+}
+HISTORY_NORMALIZATION_FLOORS = {
+    "circulation_strength_history": 1e-6, "kinetic_energy_history": 1e-8,
+    "wake_deficit_history": 1e-4, "recirculation_strength_history": 1e-5,
+    "heat_release_history": 1e-3, "peak_temperature_history": 0.1,
+    "front_position_history": 1e-5, "mid_bump_height_history": 1e-6,
+    "pressure_drop_history": 1.0,
+}
+
+
+def tolerance(name: str, value: dict[str, Any], group: str) -> dict[str, Any]:
+    kind = value.get("kind")
+    if kind == "time_history":
+        return {"kind": kind, "normalized_rmse_max": 0.06 if group == "shock_response" else 0.08,
+                "normalized_linf_max": 0.15 if group == "shock_response" else 0.20,
+                "minimum_time_coverage": 1.0,
+                "normalization_floor": HISTORY_NORMALIZATION_FLOORS.get(name, 1e-8), "provisional": True}
+    if kind == "named_profiles":
+        columns = {column for item in value.get("profiles", []) for column in item.get("columns", [])[1:]}
+        return {"kind": kind, "normalized_l1_max": 0.05 if group == "shock_response" else 0.08,
+                "normalized_linf_max": 0.15 if group == "shock_response" else 0.20,
+                "normalization_floors": {column: FIELD_NORMALIZATION_FLOORS.get(column, 1e-8) for column in sorted(columns)},
+                "criterion_role": "principal_response_shape",
+                "reference_independent": False,
+                "threshold_source": "reference_anchored_spatial_response_shape",
+                "provisional": True}
+    if kind == "profile_feature_locations":
+        return {"kind": kind, "maximum_cell_offset": 2.0, "physical_floor": 1e-10, "provisional": True}
+    raise ValueError(f"unsupported structured tolerance for {kind}")
+
+
+def uniform_scalars(path: Path) -> list[float]:
+    return [
+        float(match)
+        for match in re.findall(r"\bvalue\s+uniform\s+([-+0-9.eE]+)\s*;", read_text(path))
+    ]
+
+
+def uniform_vector_magnitudes(path: Path) -> list[float]:
+    return [
+        math.sqrt(sum(float(component) ** 2 for component in match))
+        for match in re.findall(
+            r"\bvalue\s+uniform\s+\(([-+0-9.eE]+)\s+([-+0-9.eE]+)\s+([-+0-9.eE]+)\)\s*;",
+            read_text(path),
+        )
+    ]
+
+
+def physical_tolerance(template: str, name: str, case: Path) -> dict[str, Any]:
+    common: dict[str, Any] = {
+        "kind": "physics_range",
+        "criterion_role": "principal_physics",
+        "reference_independent": True,
+    }
+    if template == "BernardCells" and name in {"temperature_min", "temperature_max"}:
+        imposed = uniform_scalars(case / "0" / "T")
+        if len(imposed) < 2:
+            raise ValueError(f"{case}: cannot determine imposed temperature envelope")
+        low, high = min(imposed), max(imposed)
+        margin = max(1e-6, 0.02 * max(high - low, 1e-6))
+        bounds = (low - margin, high + margin)
+        return {**common, "low": bounds[0], "high": bounds[1],
+                "threshold_source": "imposed_temperature_boundary_envelope", "provisional": False}
+    if template == "BernardCells" and name == "convection_mean_speed":
+        return {**common, "low": 1e-12, "high": 1e6,
+                "threshold_source": "nontrivial_buoyant_response", "provisional": True}
+    if template == "Cavity":
+        imposed = uniform_vector_magnitudes(case / "0" / "U")
+        lid_speed = max(imposed, default=0.0)
+        if lid_speed <= 0:
+            raise ValueError(f"{case}: cannot determine moving-wall speed")
+        if name == "response_speed_max":
+            return {**common, "low": 0.10 * lid_speed, "high": 1.0 * lid_speed,
+                    "threshold_source": "lid_speed_response_envelope_tightened", "provisional": True}
+        if name == "reverse_flow_min_u":
+            return {**common, "low": -1.0 * lid_speed, "high": -0.05 * lid_speed,
+                    "threshold_source": "main_vortex_reverse_flow_envelope_tightened", "provisional": True}
+    if template == "shallowWaterWithSquareBump" and name == "mid_bump_height_relative_change":
+        initial_depths = uniform_scalars(case / "0" / "h")
+        initial_depth = sum(initial_depths) / len(initial_depths) if initial_depths else 0.0
+        # The shallow-water family changes regime with its prompt-specified
+        # initial depth. A single non-zero floor would accept a numerically
+        # stagnant response for the deeper cases.
+        low = 2e-4 if initial_depth <= 0.012 else 0.1
+        return {**common, "low": low, "high": 1.0,
+                "threshold_source": "initial_depth_conditioned_bump_response", "provisional": True}
+    fixed = {
+        # These are first-stage family envelopes: they reject merely non-zero
+        # signatures while retaining the checked-in reference regimes. They
+        # are intentionally absolute and reference-independent; later runs can
+        # replace them with law-based relations or repeatability envelopes.
+        ("Cylinder", "wake_deficit_final"): (0.03, 0.15, "bounded_dimensionless_wake_deficit"),
+        ("counterFlowFlame2D", "species_sum_max_error"): (0.0, 5e-5, "species_mass_fraction_closure_tightened"),
+        ("counterFlowFlame2D", "reaction_temperature_span"): (500.0, 3000.0, "bounded_thermal_reaction_zone"),
+        ("damBreakWithObstacle", "water_volume_relative_drift"): (0.0, 5e-3, "closed_phase_volume_conservation_tightened"),
+        ("damBreakWithObstacle", "front_net_advance"): (0.03, 0.25, "bounded_downstream_free_surface_advance"),
+        ("forwardStep", "supersonic_volume_fraction"): (0.40, 1.0, "supersonic_regime_coverage_tightened"),
+        ("obliqueShock", "supersonic_volume_fraction"): (0.85, 1.0, "supersonic_regime_coverage_tightened"),
+        ("wedge", "supersonic_volume_fraction"): (0.85, 1.0, "supersonic_regime_coverage_tightened"),
+        ("Shock", "supersonic_volume_fraction"): (0.85, 1.0, "supersonic_regime_coverage_tightened"),
+        ("forwardStep", "shock_pressure_jump_ratio"): (1.50, 20.0, "bounded_compressive_pressure_feature"),
+        ("obliqueShock", "shock_pressure_jump_ratio"): (1.10, 2.20, "bounded_compressive_pressure_feature"),
+        ("wedge", "shock_pressure_jump_ratio"): (2.00, 6.50, "bounded_compressive_pressure_feature"),
+        ("Shock", "shock_pressure_jump_ratio"): (1.10, 2.20, "bounded_compressive_pressure_feature"),
+        ("pitzDaily", "reverse_flow_volume_fraction"): (1e-3, 0.08, "bounded_separated_reverse_flow_signature"),
+        ("pitzDaily", "streamwise_pressure_change_magnitude"): (8.0, 140.0, "bounded_streamwise_pressure_response"),
+        ("Obstacle", "streamwise_pressure_change_magnitude"): (0.005, 10.0, "bounded_obstacle_pressure_response"),
+        ("squareBend", "streamwise_pressure_change_magnitude"): (3e4, 1.2e5, "bounded_bend_pressure_response"),
+        ("Nozzle", "flow_speed_max"): (100.0, 1000.0, "bounded_nozzle_flow_response"),
+    }
+    if (template, name) not in fixed:
+        raise ValueError(f"no physics tolerance for {template}/{name}")
+    low, high, source = fixed[(template, name)]
+    exact_sources = {"species_mass_fraction_closure", "closed_phase_volume_conservation"}
+    return {**common, "low": low, "high": high, "threshold_source": source,
+            "provisional": source not in exact_sources}
+
+
+def diagnostic_scalar_tolerance(value: float) -> dict[str, Any]:
+    scale = max(abs(float(value)), 1e-12)
+    return {
+        "low": float(value) - 0.2 * scale,
+        "high": float(value) + 0.2 * scale,
+        "kind": "diagnostic_scalar_reference",
+        "provisional": True,
+        "threshold_source": "reference_diagnostic_relative_band",
+    }
+
+
+def build_references(run_root: Path) -> tuple[dict[str, Any], dict[str, Any]]:
+    documents: dict[str, dict[str, Any]] = {}
+    for track in ("basic", "advanced"):
+        records = {}
+        for wrapper in sorted((run_root / "materialized" / track).iterdir()):
+            case = wrapper / "case"
+            if not case.is_dir():
+                continue
+            case_id = wrapper.name.replace("__", "/", 1) if track == "basic" else wrapper.name
+            candidate = extract(case, case_id)
+            if candidate["status"] != "complete":
+                raise ValueError(f"{case_id}: {candidate['health'].get('validation_errors') or candidate['missing_metrics']}")
+            group, qois = candidate["principal_qoi_group"], candidate["qois"]
+            principal = list(principal_metrics(candidate["family"]))
+            missing_principal = sorted(set(principal) - set(qois))
+            if missing_principal:
+                raise ValueError(f"{case_id}: missing physics metrics {missing_principal}")
+            roles = {name: "principal" if name in principal else "diagnostic" for name in qois}
+            tolerances = {
+                name: tolerance(name, value, group)
+                if isinstance(value, dict) and name in principal else (
+                    physical_tolerance(candidate["family"], name, case)
+                    if name in principal else (
+                    diagnostic_scalar_tolerance(value)
+                    if isinstance(value, (int, float)) and not isinstance(value, bool)
+                    else tolerance(name, value, group)
+                    )
+                )
+                for name, value in qois.items()
+            }
+            records[case_id] = {
+                "track": track, "family": candidate["family"], "source_case_id": case_id,
+                "latest_time": candidate["latest_time"], "principal_qoi_group": group,
+                "principal_metrics": sorted(principal), "qois": qois,
+                "metric_roles": roles, "tolerances": tolerances,
+                "health": candidate["health"], "extraction": {
+                    "producer": "benchmarks/evaluation/basic_advanced.py",
+                    "geometry": "field-derived physics metrics plus physical-coordinate reference diagnostics",
+                    "reference_run": str(run_root),
+                },
+            }
+        documents[track] = {
+            "schema_version": "foambench.reference_qois.v2", "generated_at": utc_now(),
+            "openfoam_version": "Foundation v13", "producer": "benchmarks/evaluation/basic_advanced.py",
+            "design": "guide/foambench_basic_advanced_qoi_design.md",
+            "tolerance_policy": "physics_grounded_scalar_and_response_shape_joint_gate.v2",
+            "summary": {"tracks": [track], "case_count": len(records), "health_pass_count": len(records), "health_fail_count": 0},
+            "notes": ["Principal scalar QoIs are reference-independent family physics criteria extracted from retained fields.",
+                      "One existing spatial response profile per family is also principal and must jointly pass its reference-anchored shape tolerance.",
+                      "Other histories, profiles, and feature locations remain diagnostic and do not decide Physics-grounded pass.",
+                      "Provisional physical-signature and response-shape limits require future valid-alternative calibration."],
+            "cases": records,
+        }
+        validate(documents[track], "foambench_qoi_reference.schema.json")
+    return documents["basic"], documents["advanced"]
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--run-root", required=True, type=Path)
+    parser.add_argument("--basic-output", required=True, type=Path)
+    parser.add_argument("--advanced-output", required=True, type=Path)
+    args = parser.parse_args()
+    basic, advanced = build_references(args.run_root.resolve(strict=True))
+    write_json(args.basic_output, basic)
+    write_json(args.advanced_output, advanced)
+    print(json.dumps({"basic": len(basic["cases"]), "advanced": len(advanced["cases"])}, indent=2))
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/evaluation/cli.py b/benchmarks/evaluation/cli.py
new file mode 100644
index 0000000000000000000000000000000000000000..05e32d5af8fb3ec180d89e73f7a4aa4c9161302f
--- /dev/null
+++ b/benchmarks/evaluation/cli.py
@@ -0,0 +1,79 @@
+from __future__ import annotations
+
+import argparse
+import json
+import sys
+from pathlib import Path
+
+from .io import read_object
+from .models import BenchmarkProfile
+from .pipeline import evaluate_campaign
+from .preparation import prepare_campaign
+from .profiles import load_assets
+from .reporting import summary_table
+from .schema import validate
+
+
+def build_parser() -> argparse.ArgumentParser:
+    parser = argparse.ArgumentParser(description="Evaluate FoamBench rollouts with a dataset-independent scorer.")
+    subparsers = parser.add_subparsers(dest="command", required=True)
+    validate = subparsers.add_parser("validate-profile", help="validate benchmark profile assets")
+    validate.add_argument("--profile", type=Path, required=True)
+    evaluate = subparsers.add_parser("evaluate", help="evaluate one rollout campaign")
+    evaluate.add_argument("--profile", type=Path, required=True)
+    evaluate.add_argument("--adapter", choices=("easyfoam", "foamagent", "chatcfd", "coding-agent"), required=True)
+    evaluate.add_argument("--run-root", type=Path, required=True)
+    evaluate.add_argument("--output", type=Path, required=True)
+    evaluate.add_argument(
+        "--prepare", action="store_true",
+        help="generate measurement-only C, Vc, and vorticity fields before evaluation",
+    )
+    evaluate.add_argument("--prepare-jobs", type=int, default=1)
+    evaluate.add_argument(
+        "--check-mesh", action="store_true",
+        help="run read-only checkMesh when no retained mesh log is available",
+    )
+    evaluate.add_argument("--mesh-timeout", type=float, default=120.0)
+    return parser
+
+
+def main(argv: list[str] | None = None) -> int:
+    args = build_parser().parse_args(argv)
+    validate(read_object(args.profile), "benchmark_profile.schema.json")
+    profile = BenchmarkProfile.load(args.profile)
+    if args.command == "validate-profile":
+        benchmark, references = load_assets(profile)
+        print(json.dumps({
+            "profile_id": profile.profile_id,
+            "dataset": profile.dataset,
+            "benchmark_case_count": len(benchmark),
+            "reference_case_count": len(references),
+            "status": "pass",
+        }, indent=2, sort_keys=True))
+        return 0
+    if args.prepare:
+        prepare_campaign(
+            profile,
+            adapter_name=args.adapter,
+            run_root=args.run_root,
+            output_root=args.output.resolve() / "preparation",
+            jobs=args.prepare_jobs,
+        )
+    report = evaluate_campaign(
+        profile,
+        adapter_name=args.adapter,
+        run_root=args.run_root,
+        output_dir=args.output,
+        check_mesh=args.check_mesh,
+        mesh_timeout=args.mesh_timeout,
+    )
+    print(summary_table(report["overall"]))
+    return 0
+
+
+if __name__ == "__main__":
+    try:
+        raise SystemExit(main())
+    except (OSError, ValueError, RuntimeError) as exc:
+        print(f"foambench-evaluate: error: {exc}", file=sys.stderr)
+        raise SystemExit(2)
diff --git a/benchmarks/evaluation/comparison.py b/benchmarks/evaluation/comparison.py
new file mode 100644
index 0000000000000000000000000000000000000000..946206e34623d1714b26ab564f3232b6d2263ced
--- /dev/null
+++ b/benchmarks/evaluation/comparison.py
@@ -0,0 +1,750 @@
+#!/usr/bin/env python3
+"""Compare candidate FoamBench QoIs with checked-in reference contracts.
+
+Coverage and numerical agreement are reported separately. Related field
+statistics are scored as equal-weight QoI groups; ranges and runtime metrics
+remain available as diagnostics but do not determine the group score. A
+missing QoI means that the benchmark cannot assess that part of the result; it
+is not relabelled as an out-of-tolerance value.
+"""
+from __future__ import annotations
+
+import argparse
+import json
+import math
+import re
+import sys
+from datetime import datetime, timezone
+from pathlib import Path
+from typing import Any
+
+
+def finite(value: Any) -> float | None:
+    if isinstance(value, bool) or not isinstance(value, (int, float)):
+        return None
+    result = float(value)
+    return result if math.isfinite(result) else None
+
+
+def scalar_observation(value: Any) -> float | None:
+    direct = finite(value)
+    if direct is not None:
+        return direct
+    if isinstance(value, dict) and value.get("kind") in {"scalar_ratio", "window_regression"}:
+        return finite(value.get("value"))
+    return None
+
+
+def interpolate(points: list[dict[str, Any]], time: float) -> float | None:
+    rows = [(finite(item.get("time")), finite(item.get("value"))) for item in points if isinstance(item, dict)]
+    rows = sorted((t, v) for t, v in rows if t is not None and v is not None)
+    if not rows or time < rows[0][0] or time > rows[-1][0]:
+        return None
+    for index, (left_t, left_v) in enumerate(rows):
+        if abs(time - left_t) <= 1e-12 * max(1.0, abs(time)):
+            return left_v
+        if index + 1 < len(rows) and left_t < time < rows[index + 1][0]:
+            right_t, right_v = rows[index + 1]
+            weight = (time - left_t) / (right_t - left_t)
+            return left_v + weight * (right_v - left_v)
+    return None
+
+
+def compare_history(reference: dict[str, Any], candidate: dict[str, Any], tolerance: dict[str, Any]) -> dict[str, Any]:
+    reference_points = reference.get("points", [])
+    candidate_points = candidate.get("points", [])
+    pairs = []
+    for point in reference_points if isinstance(reference_points, list) else []:
+        time, reference_value = finite(point.get("time")), finite(point.get("value")) if isinstance(point, dict) else (None, None)
+        if time is None or reference_value is None:
+            continue
+        candidate_value = interpolate(candidate_points if isinstance(candidate_points, list) else [], time)
+        if candidate_value is not None:
+            pairs.append((reference_value, candidate_value))
+    required_coverage = finite(tolerance.get("minimum_time_coverage")) or 1.0
+    coverage = len(pairs) / len(reference_points) if reference_points else 0.0
+    if not pairs:
+        return {"status": "missing", "coverage_fraction": coverage}
+    floor = finite(tolerance.get("normalization_floor")) or 1e-12
+    norm = max(math.sqrt(sum(ref * ref for ref, _ in pairs) / len(pairs)), floor)
+    errors = [cand - ref for ref, cand in pairs]
+    nrmse = math.sqrt(sum(error * error for error in errors) / len(errors)) / norm
+    nlinf = max(abs(error) for error in errors) / norm
+    rmse_limit = finite(tolerance.get("normalized_rmse_max"))
+    linf_limit = finite(tolerance.get("normalized_linf_max"))
+    valid = rmse_limit is not None and linf_limit is not None
+    passed = valid and coverage >= required_coverage and nrmse <= rmse_limit and nlinf <= linf_limit
+    return {"status": "within_tolerance" if passed else "invalid_contract" if not valid else "out_of_tolerance",
+            "coverage_fraction": coverage, "aligned_point_count": len(pairs),
+            "normalized_rmse": nrmse, "normalized_linf": nlinf,
+            "normalized_rmse_max": rmse_limit, "normalized_linf_max": linf_limit}
+
+
+def profile_key(profile: dict[str, Any]) -> str:
+    """Normalize centerline aliases by the coordinate direction they sample."""
+    name = Path(str(profile.get("profile_id", ""))).name.lower()
+    stem = Path(name).stem
+    if stem in {"centreline_y0", "centerline_y0", "centerliney", "horizontal", "horizontalcenterline", "horizontalcentreline"}:
+        return "horizontal.xy"
+    if stem in {"centreline_x0", "centerline_x0", "centerlinex", "vertical", "verticalcenterline", "verticalcentreline"}:
+        return "vertical.xy"
+    return name
+
+
+def compare_profiles(reference: dict[str, Any], candidate: dict[str, Any], tolerance: dict[str, Any]) -> dict[str, Any]:
+    references = {profile_key(item): item for item in reference.get("profiles", []) if isinstance(item, dict)}
+    candidates = {profile_key(item): item for item in candidate.get("profiles", []) if isinstance(item, dict)}
+    l1_limit, linf_limit = finite(tolerance.get("normalized_l1_max")), finite(tolerance.get("normalized_linf_max"))
+    if l1_limit is None or linf_limit is None:
+        return {"status": "invalid_contract"}
+    fields: list[dict[str, Any]] = []
+    expected_fields = sum(max(0, len(item.get("columns", [])) - 1) for item in references.values())
+    for key, ref_profile in references.items():
+        cand_profile = candidates.get(key)
+        if cand_profile is None:
+            continue
+        ref_columns, cand_columns = ref_profile.get("columns", []), cand_profile.get("columns", [])
+        ref_rows, cand_rows = ref_profile.get("rows", []), cand_profile.get("rows", [])
+        if len(ref_columns) < 2 or ref_columns[0] not in cand_columns:
+            continue
+        cand_x = cand_columns.index(ref_columns[0])
+        for field in ref_columns[1:]:
+            if field not in cand_columns:
+                continue
+            ref_i, cand_i = ref_columns.index(field), cand_columns.index(field)
+            cand_points = [{"time": row[cand_x], "value": row[cand_i]} for row in cand_rows]
+            pairs = [(row[ref_i], interpolate(cand_points, row[0])) for row in ref_rows]
+            pairs = [(ref, cand) for ref, cand in pairs if finite(ref) is not None and cand is not None]
+            if not pairs:
+                continue
+            declared_floors = tolerance.get("normalization_floors", {})
+            field_floor = finite(declared_floors.get(field)) if isinstance(declared_floors, dict) else None
+            norm = max(sum(abs(ref) for ref, _ in pairs) / len(pairs), field_floor or finite(tolerance.get("normalization_floor")) or 1e-12)
+            errors = [abs(cand - ref) for ref, cand in pairs]
+            fields.append({"profile": key, "field": field, "normalized_l1": sum(errors) / len(errors) / norm,
+                           "normalized_linf": max(errors) / norm})
+    coverage = len(fields) / expected_fields if expected_fields else 0.0
+    passed = bool(fields) and coverage == 1.0 and all(item["normalized_l1"] <= l1_limit and item["normalized_linf"] <= linf_limit for item in fields)
+    return {"status": "within_tolerance" if passed else "missing" if not fields else "out_of_tolerance",
+            "coverage_fraction": coverage, "observed_field_count": len(fields),
+            "expected_field_count": expected_fields, "fields": fields,
+            "normalized_l1_max": l1_limit, "normalized_linf_max": linf_limit}
+
+
+def compare_events(reference: dict[str, Any], candidate: dict[str, Any], tolerance: dict[str, Any]) -> dict[str, Any]:
+    def groups(value: dict[str, Any]) -> dict[tuple[str, str], list[dict[str, Any]]]:
+        result: dict[tuple[str, str], list[dict[str, Any]]] = {}
+        for event in value.get("events", []):
+            if isinstance(event, dict):
+                result.setdefault((profile_key({"profile_id": event.get("profile_id", "")}), str(event.get("field"))), []).append(event)
+        return result
+    refs, cands = groups(reference), groups(candidate)
+    cell_limit = finite(tolerance.get("maximum_cell_offset"))
+    if cell_limit is None:
+        return {"status": "invalid_contract"}
+    offsets = []
+    for key, ref_events in refs.items():
+        cand_events = cands.get(key, [])
+        available = list(cand_events)
+        for event in ref_events:
+            coordinate = finite(event.get("coordinate"))
+            if coordinate is None or not available:
+                continue
+            match = min(
+                available,
+                key=lambda item: abs(value - coordinate) if (value := finite(item.get("coordinate"))) is not None else math.inf,
+            )
+            available.remove(match)
+            matched_coordinate = finite(match.get("coordinate"))
+            if matched_coordinate is None:
+                continue
+            cell = max(finite(event.get("local_cell_size")) or 0.0, finite(match.get("local_cell_size")) or 0.0,
+                       finite(tolerance.get("physical_floor")) or 1e-12)
+            offsets.append(abs(matched_coordinate - coordinate) / cell)
+    expected = sum(len(items) for items in refs.values())
+    coverage = len(offsets) / expected if expected else 0.0
+    passed = expected > 0 and coverage == 1.0 and max(offsets, default=math.inf) <= cell_limit
+    return {"status": "within_tolerance" if passed else "missing" if not offsets else "out_of_tolerance",
+            "coverage_fraction": coverage, "maximum_cell_offset": max(offsets, default=None), "allowed_cell_offset": cell_limit}
+
+
+def compare_structured(reference: dict[str, Any], candidate: Any, tolerance: dict[str, Any]) -> dict[str, Any]:
+    if not isinstance(candidate, dict) or candidate.get("kind") != reference.get("kind"):
+        return {"status": "missing"}
+    kind = reference.get("kind")
+    if kind == "time_history":
+        return compare_history(reference, candidate, tolerance)
+    if kind == "branched_time_histories":
+        ref_branches, cand_branches = reference.get("branches", {}), candidate.get("branches", {})
+        results = {name: compare_history(value, cand_branches.get(name, {}), tolerance)
+                   for name, value in ref_branches.items()}
+        passed = bool(results) and all(item["status"] == "within_tolerance" for item in results.values())
+        return {"status": "within_tolerance" if passed else "out_of_tolerance", "branches": results,
+                "coverage_fraction": sum(item.get("coverage_fraction", 0.0) for item in results.values()) / len(results) if results else 0.0}
+    if kind == "named_profiles":
+        return compare_profiles(reference, candidate, tolerance)
+    if kind == "profile_feature_locations":
+        return compare_events(reference, candidate, tolerance)
+    if kind == "component_trajectory":
+        refs = {str(item.get("component_id")): item for item in reference.get("series", [])}
+        cands = {str(item.get("component_id")): item for item in candidate.get("series", [])}
+        results = {key: compare_history({"points": item.get("points", [])}, {"points": cands.get(key, {}).get("points", [])}, tolerance)
+                   for key, item in refs.items()}
+        passed = bool(results) and all(item["status"] == "within_tolerance" for item in results.values())
+        return {"status": "within_tolerance" if passed else "out_of_tolerance", "components": results}
+    if kind == "component_scalars":
+        refs = {str(item.get("component_id")): finite(item.get("value")) for item in reference.get("components", [])}
+        cands = {str(item.get("component_id")): finite(item.get("value")) for item in candidate.get("components", [])}
+        relative, floor = finite(tolerance.get("relative_max")), finite(tolerance.get("absolute_floor")) or 1e-12
+        if relative is None:
+            return {"status": "invalid_contract"}
+        errors = {key: abs(cands[key] - ref) / max(abs(ref), floor) for key, ref in refs.items() if ref is not None and cands.get(key) is not None}
+        physical_low, physical_high = finite(tolerance.get("physical_low")), finite(tolerance.get("physical_high"))
+        observed = [value for value in cands.values() if value is not None]
+        physically_valid = all(
+            (physical_low is None or value >= physical_low)
+            and (physical_high is None or value <= physical_high)
+            for value in observed
+        )
+        passed = len(errors) == len(refs) and physically_valid and all(error <= relative for error in errors.values())
+        return {"status": "within_tolerance" if passed else "missing" if not errors else "out_of_tolerance",
+                "relative_errors": errors, "physical_bounds_pass": physically_valid,
+                "physical_low": physical_low, "physical_high": physical_high}
+    if kind == "branch_scalars":
+        ref_branches, cand_branches = reference.get("branches", {}), candidate.get("branches", {})
+        relative, floor = finite(tolerance.get("relative_max")), finite(tolerance.get("absolute_floor")) or 1e-12
+        if relative is None:
+            return {"status": "invalid_contract"}
+        errors: dict[str, Any] = {}
+        for branch, ref_metrics in ref_branches.items():
+            cand_metrics = cand_branches.get(branch, {})
+            errors[branch] = {
+                name: abs(float(cand_metrics[name]) - float(ref)) / max(abs(float(ref)), floor)
+                for name, ref in ref_metrics.items()
+                if name in cand_metrics and finite(ref) is not None and finite(cand_metrics[name]) is not None
+            }
+        complete = set(errors) == set(ref_branches) and all(set(errors[b]) == set(ref_branches[b]) for b in ref_branches)
+        physical_low, physical_high = finite(tolerance.get("physical_low")), finite(tolerance.get("physical_high"))
+        observed = [value for branch in cand_branches.values() if isinstance(branch, dict) for value in branch.values()
+                    if finite(value) is not None]
+        physically_valid = all(
+            (physical_low is None or float(value) >= physical_low)
+            and (physical_high is None or float(value) <= physical_high)
+            for value in observed
+        )
+        passed = complete and physically_valid and all(error <= relative for branch in errors.values() for error in branch.values())
+        return {"status": "within_tolerance" if passed else "missing" if not complete else "out_of_tolerance",
+                "relative_errors": errors, "relative_max": relative,
+                "physical_bounds_pass": physically_valid, "physical_low": physical_low,
+                "physical_high": physical_high}
+    scalar_ref, scalar_cand = scalar_observation(reference), scalar_observation(candidate)
+    if scalar_ref is not None and scalar_cand is not None:
+        relative, floor = finite(tolerance.get("relative_max")), finite(tolerance.get("absolute_floor")) or 1e-12
+        if relative is None:
+            return {"status": "invalid_contract"}
+        error = abs(scalar_cand - scalar_ref) / max(abs(scalar_ref), floor)
+        physical_low, physical_high = finite(tolerance.get("physical_low")), finite(tolerance.get("physical_high"))
+        physically_valid = (
+            (physical_low is None or scalar_cand >= physical_low)
+            and (physical_high is None or scalar_cand <= physical_high)
+        )
+        passed = error <= relative and physically_valid
+        return {"status": "within_tolerance" if passed else "out_of_tolerance",
+                "relative_error": error, "relative_max": relative, "physical_bounds_pass": physically_valid,
+                "physical_low": physical_low, "physical_high": physical_high}
+    return {"status": "invalid_contract", "reason": f"unsupported structured kind {kind!r}"}
+
+
+def comparison_quality(result: dict[str, Any]) -> float:
+    """Map comparison distance to [0, 1] without changing strict status."""
+    status = result.get("status")
+    if status == "within_tolerance":
+        return 1.0
+    if status in {"missing", "invalid_contract"}:
+        return 0.0
+    distances: list[float] = []
+    for key in ("relative_error", "normalized_rmse", "normalized_l1", "maximum_cell_offset"):
+        value = finite(result.get(key))
+        limit = finite(result.get({
+            "relative_error": "relative_max",
+            "normalized_rmse": "normalized_rmse_max",
+            "normalized_l1": "normalized_l1_max",
+            "maximum_cell_offset": "allowed_cell_offset",
+        }[key]))
+        if value is not None and limit is not None and limit > 0:
+            distances.append(value / limit)
+    for value in result.get("fields", []) if isinstance(result.get("fields"), list) else []:
+        if isinstance(value, dict):
+            q = comparison_quality({
+                "status": "within_tolerance" if value.get("normalized_l1", math.inf) <= (result.get("normalized_l1_max") or 0.0) else "out_of_tolerance",
+                "normalized_l1": value.get("normalized_l1"),
+                "normalized_l1_max": result.get("normalized_l1_max"),
+            })
+            distances.append(1.0 - q)
+    for value in result.get("branches", {}).values() if isinstance(result.get("branches"), dict) else []:
+        if isinstance(value, dict):
+            distances.append(1.0 - comparison_quality(value))
+    ratio = sum(distances) / len(distances) if distances else 1.0
+    return max(0.0, min(1.0, 1.0 / (1.0 + ratio)))
+
+
+def load_cases(path: Path) -> dict[str, Any]:
+    data = json.loads(path.read_text(encoding="utf-8"))
+    cases = data.get("cases") if isinstance(data, dict) else None
+    if not isinstance(cases, dict):
+        raise ValueError(f"JSON has no cases object: {path}")
+    return cases
+
+
+def write_json(path: Path, value: Any) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    temporary.write_text(json.dumps(value, ensure_ascii=False, indent=2, sort_keys=True) + "\n", encoding="utf-8")
+    temporary.replace(path)
+
+
+STAT_SUFFIX_RE = re.compile(r"_(?:min|max|mean|range)$")
+SCORING_POLICY = "grouped_qois"
+EXPLICIT_SCORING_POLICY = "explicit_principal_qoi_group"
+
+
+def case_scoring_policy(reference: dict[str, Any]) -> str:
+    return EXPLICIT_SCORING_POLICY if isinstance(reference.get("metric_roles"), dict) else SCORING_POLICY
+
+
+def metric_role(name: str, explicit_roles: dict[str, Any] | None = None) -> str:
+    """Classify metrics without changing the extracted raw values.
+
+    Residual and Courant values remain useful diagnostics, while ``range`` is
+    a deterministic derivative of min/max.  All other legacy measurements are
+    scored, but related statistics are aggregated as one QoI group below.
+    """
+    explicit = explicit_roles.get(name) if explicit_roles else None
+    if explicit in {"principal", "scored"}:
+        return "scored"
+    if explicit in {"diagnostic", "redundant"}:
+        return explicit
+    if "residual" in name or "courant" in name:
+        return "diagnostic"
+    if name.endswith("_range"):
+        return "redundant"
+    return "scored"
+
+
+def metric_group(name: str, principal_group: str | None = None,
+                 explicit_roles: dict[str, Any] | None = None) -> str:
+    if principal_group and explicit_roles and explicit_roles.get(name) in {"principal", "scored"}:
+        return principal_group
+    if name in {"center_u", "center_v", "center_w", "center_speed"}:
+        return "center_velocity"
+    return STAT_SUFFIX_RE.sub("", name)
+
+
+def comparison_outcome(*, missing: list[str], out_of_tolerance: list[str],
+                       invalid_contract: list[str], accepted: bool) -> str:
+    if invalid_contract:
+        return "invalid_contract"
+    if accepted:
+        return "pass"
+    if missing and out_of_tolerance:
+        return "incomplete_and_out_of_tolerance"
+    if missing:
+        return "incomplete"
+    return "out_of_tolerance"
+
+
+def rollout_status(comparison: dict[str, Any]) -> str:
+    """Map a QoI result to a rollout status after execution has passed."""
+    return {
+        "pass": "scientifically_validated",
+        "incomplete": "execution_passed_qoi_incomplete",
+        "out_of_tolerance": "execution_passed_qoi_out_of_tolerance",
+        "incomplete_and_out_of_tolerance": "execution_passed_qoi_incomplete_and_out_of_tolerance",
+        "invalid_contract": "execution_passed_qoi_evaluation_error",
+        "error": "execution_passed_qoi_evaluation_error",
+    }.get(str(comparison.get("status")), "execution_passed_qoi_evaluation_error")
+
+
+def compare_case(reference: dict[str, Any], candidate: dict[str, Any], required_fraction: float) -> dict[str, Any]:
+    references = reference.get("qois") if isinstance(reference.get("qois"), dict) else {}
+    tolerances = reference.get("tolerances") if isinstance(reference.get("tolerances"), dict) else {}
+    candidates = candidate.get("qois") if isinstance(candidate.get("qois"), dict) else {}
+    explicit_roles = reference.get("metric_roles") if isinstance(reference.get("metric_roles"), dict) else None
+    principal_group = reference.get("principal_qoi_group") if isinstance(reference.get("principal_qoi_group"), str) else None
+    role_for = lambda name: metric_role(name, explicit_roles)
+    metrics: dict[str, Any] = {}
+    passed = 0
+    out_of_tolerance: list[str] = []
+    missing: list[str] = []
+    invalid_contract: list[str] = []
+    diagnostic_out_of_tolerance: list[str] = []
+    diagnostic_missing: list[str] = []
+    redundant_metric_count = 0
+    groups: dict[str, dict[str, Any]] = {}
+    for name, reference_value in sorted(references.items()):
+        role = role_for(name)
+        group = metric_group(name, principal_group, explicit_roles)
+        if role == "redundant":
+            redundant_metric_count += 1
+            value = finite(candidates.get(name))
+            metrics[name] = {
+                "status": "available" if value is not None else "missing",
+                "role": role,
+                "group": group,
+                "reference_value": reference_value,
+                "candidate_value": value,
+            }
+            continue
+        group_record = groups.setdefault(group, {
+            "role": "scored" if role == "scored" else role,
+            "metrics": [],
+            "passed_metric_count": 0,
+            "observed_metric_count": 0,
+            "invalid_metric_count": 0,
+            "quality_sum": 0.0,
+            "coverage_fraction": 1.0,
+        })
+        group_record["metrics"].append(name)
+        tolerance = tolerances.get(name) if isinstance(tolerances.get(name), dict) else {}
+        if isinstance(reference_value, dict):
+            result = compare_structured(reference_value, candidates.get(name), tolerance)
+            result["quality"] = comparison_quality(result)
+            status = result.get("status")
+            is_missing = status == "missing"
+            is_invalid = status == "invalid_contract"
+            is_pass = status == "within_tolerance"
+            structured_coverage = finite(result.get("coverage_fraction"))
+            if structured_coverage is not None:
+                group_record["coverage_fraction"] = min(
+                    group_record["coverage_fraction"], structured_coverage
+                )
+            elif is_missing:
+                group_record["coverage_fraction"] = 0.0
+            if is_missing:
+                missing.append(name)
+                if role == "diagnostic":
+                    diagnostic_missing.append(name)
+            elif is_invalid and role == "scored":
+                invalid_contract.append(name)
+                group_record["invalid_metric_count"] += 1
+            else:
+                group_record["observed_metric_count"] += int(role == "scored")
+                if role == "scored":
+                    passed += int(is_pass)
+                    group_record["passed_metric_count"] += int(is_pass)
+                    group_record["quality_sum"] += float(result["quality"])
+                    if not is_pass:
+                        out_of_tolerance.append(name)
+                elif role == "diagnostic" and not is_pass:
+                    diagnostic_out_of_tolerance.append(name)
+            metrics[name] = {"role": role, "group": group, "reference_value": reference_value,
+                             "candidate_value": candidates.get(name), **result}
+            continue
+        value = finite(candidates.get(name))
+        low, high = finite(tolerance.get("low")), finite(tolerance.get("high"))
+        if value is None:
+            missing.append(name)
+            group_record["coverage_fraction"] = 0.0
+            if role == "diagnostic":
+                diagnostic_missing.append(name)
+            metrics[name] = {
+                "status": "missing",
+                "role": role,
+                "group": group,
+                "reference_value": reference_value,
+                "quality": 0.0,
+            }
+            continue
+        if low is None or high is None:
+            group_record["coverage_fraction"] = 0.0
+            if role == "scored":
+                invalid_contract.append(name)
+                group_record["invalid_metric_count"] += 1
+            metrics[name] = {
+                "status": "invalid_contract" if role == "scored" else "available_without_tolerance",
+                "role": role,
+                "group": group,
+                "reference_value": reference_value,
+                "candidate_value": value,
+                "quality": 0.0,
+            }
+            continue
+        physical_low, physical_high = finite(tolerance.get("physical_low")), finite(tolerance.get("physical_high"))
+        physical_pass = (
+            (physical_low is None or value >= physical_low)
+            and (physical_high is None or value <= physical_high)
+        )
+        is_pass = low <= value <= high and physical_pass
+        tolerance_span = max(high - low, 1e-12)
+        distance = 0.0 if is_pass else min(abs(value - min(max(value, low), high)) / tolerance_span, 1.0)
+        quality = 1.0 if is_pass else max(0.0, 1.0 - distance)
+        if role == "scored":
+            passed += int(is_pass)
+            group_record["observed_metric_count"] += 1
+            group_record["passed_metric_count"] += int(is_pass)
+            group_record["quality_sum"] += quality
+            if not is_pass:
+                out_of_tolerance.append(name)
+        elif role == "diagnostic" and not is_pass:
+            diagnostic_out_of_tolerance.append(name)
+        metrics[name] = {
+            "status": "within_tolerance" if is_pass else "out_of_tolerance",
+            "role": role,
+            "group": group,
+            "reference_value": reference_value,
+            "candidate_value": value,
+            "low": low,
+            "high": high,
+            "absolute_error": abs(value - float(reference_value)),
+            "criterion_role": tolerance.get("criterion_role"),
+            "threshold_source": tolerance.get("threshold_source"),
+            "reference_independent": tolerance.get("reference_independent", False),
+            "provisional": tolerance.get("provisional"),
+            "physical_bounds_pass": physical_pass,
+            "physical_low": physical_low,
+            "physical_high": physical_high,
+            "physical_threshold_source": tolerance.get("physical_threshold_source"),
+            "quality": quality,
+        }
+    scored_groups = {
+        name: record for name, record in groups.items() if record["role"] == "scored"
+    }
+    scored_metrics = [name for name in references if role_for(name) == "scored"]
+    scored_missing = [name for name in missing if role_for(name) == "scored"]
+    scored_count = len(scored_metrics)
+    extracted_count = sum(record["observed_metric_count"] for record in scored_groups.values())
+    evaluated_count = extracted_count
+    coverage = extracted_count / scored_count if scored_count else 0.0
+    metric_value_pass_fraction = passed / evaluated_count if evaluated_count else None
+    metric_joint_pass_fraction = passed / scored_count if scored_count else 0.0
+    group_scores: dict[str, dict[str, Any]] = {}
+    for group_name, record in sorted(scored_groups.items()):
+        member_count = len(record["metrics"])
+        group_score = record["quality_sum"] / member_count if member_count else 0.0
+        group_coverage = (
+            min(record["observed_metric_count"] / member_count, record["coverage_fraction"])
+            if member_count else 0.0
+        )
+        group_scores[group_name] = {
+            "score": group_score,
+            "coverage_fraction": group_coverage,
+            "metric_count": member_count,
+            "observed_metric_count": record["observed_metric_count"],
+            "passed_metric_count": record["passed_metric_count"],
+            "metrics": record["metrics"],
+        }
+    qoi_pass_ratio = (
+        sum(item["score"] for item in group_scores.values()) / len(group_scores)
+        if group_scores else 0.0
+    )
+    qoi_coverage_fraction = (
+        sum(item["coverage_fraction"] for item in group_scores.values()) / len(group_scores)
+        if group_scores else 0.0
+    )
+    # Continuous quality is intentionally separate from the strict scientific
+    # acceptance bit.  It exposes partial QoI agreement to Evolution without
+    # weakening the all-groups physics-grounded contract.
+    qoi_quality = qoi_pass_ratio * qoi_coverage_fraction
+    physics_grounded_accepted = bool(
+        scored_groups
+        and not scored_missing
+        and not invalid_contract
+        and not out_of_tolerance
+        and passed == scored_count
+        and all(
+            item["coverage_fraction"] == 1.0
+            for item in group_scores.values()
+        )
+    )
+    threshold_pass = bool(
+        scored_groups
+        and qoi_coverage_fraction == 1.0
+        and qoi_pass_ratio >= required_fraction
+    )
+    outcome = comparison_outcome(
+        missing=scored_missing,
+        out_of_tolerance=out_of_tolerance,
+        invalid_contract=invalid_contract,
+        accepted=physics_grounded_accepted,
+    )
+    diagnostic_names = [name for name in references if role_for(name) == "diagnostic"]
+    diagnostic_observed = [
+        name for name in diagnostic_names
+        if metrics.get(name, {}).get("status") not in {None, "missing", "invalid_contract"}
+    ]
+    diagnostic_passed = [
+        name for name in diagnostic_names if metrics.get(name, {}).get("status") == "within_tolerance"
+    ]
+    return {
+        "schema_version": "foambench.qoi.case_comparison.v3",
+        "scoring_policy": case_scoring_policy(reference),
+        "status": outcome,
+        "coverage_status": "complete" if scored_count and not scored_missing else "incomplete",
+        "value_status": (
+            "not_assessed" if not scored_count
+            else "within_tolerance" if metric_value_pass_fraction is not None and metric_value_pass_fraction >= required_fraction
+            else "out_of_tolerance"
+        ),
+        "required_metric_count": scored_count,
+        "extracted_metric_count": extracted_count,
+        "evaluated_metric_count": evaluated_count,
+        "passed_metric_count": passed,
+        "coverage_fraction": coverage,
+        "value_pass_fraction": metric_value_pass_fraction,
+        "joint_pass_fraction": metric_joint_pass_fraction,
+        "qoi_pass_ratio": qoi_pass_ratio,
+        "qoi_quality": qoi_quality,
+        "qoi_coverage_fraction": qoi_coverage_fraction,
+        "group_count": len(group_scores),
+        "group_scores": group_scores,
+        "physics_grounded_qoi_pass": physics_grounded_accepted,
+        "threshold_pass": threshold_pass,
+        "diagnostic_metric_count": sum(len(record["metrics"]) for record in groups.values() if record["role"] == "diagnostic"),
+        "diagnostic_observed_metric_count": len(diagnostic_observed),
+        "diagnostic_passed_metric_count": len(diagnostic_passed),
+        "diagnostic_reference_coverage_fraction": (
+            len(diagnostic_observed) / len(diagnostic_names) if diagnostic_names else None
+        ),
+        "diagnostic_reference_pass_fraction": (
+            len(diagnostic_passed) / len(diagnostic_observed) if diagnostic_observed else None
+        ),
+        "redundant_metric_count": redundant_metric_count,
+        # Raw metric fractions remain available above; the canonical case-level
+        # quality score is qoi_pass_ratio.
+        "pass_fraction": metric_joint_pass_fraction,
+        "required_fraction": required_fraction,
+        "missing_metrics": missing,
+        "scored_missing_metrics": scored_missing,
+        "diagnostic_missing_metrics": diagnostic_missing,
+        "out_of_tolerance_metrics": out_of_tolerance,
+        "diagnostic_out_of_tolerance_metrics": diagnostic_out_of_tolerance,
+        "invalid_contract_metrics": invalid_contract,
+        "metrics": metrics,
+    }
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--reference-qois", required=True, type=Path)
+    parser.add_argument("--candidate-qois", required=True, type=Path)
+    parser.add_argument("--case-id", action="append")
+    parser.add_argument(
+        "--required-fraction",
+        type=float,
+        default=1.0,
+        help="Optional observed-value/QoI-ratio threshold; physics_grounded_qoi_pass always requires every scored group.",
+    )
+    parser.add_argument("--output", type=Path)
+    parser.add_argument("--json", action="store_true")
+    args = parser.parse_args()
+    if not 0 < args.required_fraction <= 1:
+        parser.error("--required-fraction must be in (0, 1]")
+
+    references = load_cases(args.reference_qois.resolve(strict=True))
+    candidates = load_cases(args.candidate_qois.resolve(strict=True))
+    selected = args.case_id or sorted(references)
+    unknown = sorted(set(selected) - set(references))
+    if unknown:
+        raise ValueError("unknown reference case IDs: " + ", ".join(unknown))
+
+    results: dict[str, Any] = {}
+    missing_cases: list[str] = []
+    for case_id in selected:
+        candidate = candidates.get(case_id)
+        if not isinstance(candidate, dict):
+            missing_cases.append(case_id)
+            missing_metrics = sorted(references[case_id].get("qois", {}))
+            results[case_id] = {
+                "scoring_policy": case_scoring_policy(references[case_id]),
+                "status": "missing_candidate_case",
+                "coverage_status": "incomplete",
+                "value_status": "not_assessed",
+                "required_metric_count": len(missing_metrics),
+                "extracted_metric_count": 0,
+                "evaluated_metric_count": 0,
+                "passed_metric_count": 0,
+                "coverage_fraction": 0.0,
+                "value_pass_fraction": None,
+                "joint_pass_fraction": 0.0,
+                "qoi_pass_ratio": 0.0,
+                "qoi_coverage_fraction": 0.0,
+                "group_count": 0,
+                "pass_fraction": 0.0,
+                "missing_metrics": missing_metrics,
+                "out_of_tolerance_metrics": [],
+                "invalid_contract_metrics": [],
+            }
+        else:
+            results[case_id] = compare_case(references[case_id], candidate, args.required_fraction)
+
+    family_rows: dict[str, list[dict[str, Any]]] = {}
+    for case_id, result in results.items():
+        if "pass_fraction" in result:
+            reference_family = references.get(case_id, {}).get("family")
+            family = reference_family if isinstance(reference_family, str) and reference_family else case_id.split("/", 1)[0]
+            family_rows.setdefault(family, []).append(result)
+    def summarize(rows: list[dict[str, Any]]) -> dict[str, Any]:
+        assessed = [row["value_pass_fraction"] for row in rows if row.get("value_pass_fraction") is not None]
+        qoi_ratios = [row["qoi_pass_ratio"] for row in rows if row.get("qoi_pass_ratio") is not None]
+        return {
+            "case_count": len(rows),
+            "passed_case_count": sum(row["status"] == "pass" for row in rows),
+            "incomplete_case_count": sum(bool(row.get("missing_metrics")) for row in rows),
+            "out_of_tolerance_case_count": sum(bool(row.get("out_of_tolerance_metrics")) for row in rows),
+            "macro_coverage_fraction": sum(row["coverage_fraction"] for row in rows) / len(rows),
+            "macro_value_pass_fraction": sum(assessed) / len(assessed) if assessed else None,
+            "macro_joint_pass_fraction": sum(row["joint_pass_fraction"] for row in rows) / len(rows),
+            "macro_qoi_pass_ratio": sum(qoi_ratios) / len(qoi_ratios) if qoi_ratios else 0.0,
+            "macro_qoi_coverage_fraction": sum(row.get("qoi_coverage_fraction", 0.0) for row in rows) / len(rows),
+        }
+
+    families = {family: summarize(rows) for family, rows in sorted(family_rows.items())}
+    passed_cases = sum(result.get("status") == "pass" for result in results.values())
+    aggregate = summarize(list(results.values())) if results else {
+        "incomplete_case_count": 0,
+        "out_of_tolerance_case_count": 0,
+        "macro_coverage_fraction": 0.0,
+        "macro_value_pass_fraction": None,
+        "macro_joint_pass_fraction": 0.0,
+        "macro_qoi_pass_ratio": 0.0,
+        "macro_qoi_coverage_fraction": 0.0,
+    }
+    policies = {result.get("scoring_policy", SCORING_POLICY) for result in results.values()}
+    report = {
+        "schema_version": "foambench.qoi.comparison.v3",
+        "scoring_policy": policies.pop() if len(policies) == 1 else "mixed",
+        "generated_at": datetime.now(timezone.utc).isoformat(),
+        "status": "pass" if passed_cases == len(selected) and not missing_cases else "fail",
+        "case_count": len(selected),
+        "passed_case_count": passed_cases,
+        "case_pass_fraction": passed_cases / len(selected) if selected else 0.0,
+        "incomplete_case_count": aggregate["incomplete_case_count"],
+        "out_of_tolerance_case_count": aggregate["out_of_tolerance_case_count"],
+        "macro_coverage_fraction": aggregate["macro_coverage_fraction"],
+        "macro_value_pass_fraction": aggregate["macro_value_pass_fraction"],
+        "macro_joint_pass_fraction": aggregate["macro_joint_pass_fraction"],
+        "macro_qoi_pass_ratio": aggregate["macro_qoi_pass_ratio"],
+        "macro_qoi_coverage_fraction": aggregate["macro_qoi_coverage_fraction"],
+        "missing_cases": missing_cases,
+        "families": families,
+        "cases": results,
+    }
+    if args.output:
+        write_json(args.output.resolve(), report)
+    if args.json or not args.output:
+        print(json.dumps(report, ensure_ascii=False, indent=2, sort_keys=True))
+    else:
+        print(
+            f"comparison: {args.output.resolve()} "
+            f"(physics_grounded={passed_cases}/{len(selected)}, "
+            f"qoi_pass_ratio={report['macro_qoi_pass_ratio']:.4f})"
+        )
+    return 0 if report["status"] == "pass" else 1
+
+
+if __name__ == "__main__":
+    try:
+        raise SystemExit(main())
+    except (OSError, ValueError, json.JSONDecodeError) as exc:
+        print(f"compare_foambench_qois.py: error: {exc}", file=sys.stderr)
+        raise SystemExit(2)
diff --git a/benchmarks/evaluation/evidence_contract.py b/benchmarks/evaluation/evidence_contract.py
new file mode 100644
index 0000000000000000000000000000000000000000..cb01f7bc6559afc5e470de7f42607d8d7a08c593
--- /dev/null
+++ b/benchmarks/evaluation/evidence_contract.py
@@ -0,0 +1,119 @@
+"""Canonical evidence discovery for the Extended FoamBench contract.
+
+The resolver deliberately separates *where/how an agent writes a file* from
+the physical quantity represented by its contents.  Callers still validate
+headers, units, time semantics, and dimensions before using a file as QoI
+evidence; this module only provides deterministic semantic routing.
+"""
+from __future__ import annotations
+
+import re
+import json
+from pathlib import Path
+from typing import Any
+
+
+CANONICAL_ALIASES: dict[str, tuple[str, ...]] = {
+    "force_coefficients": ("forcecoeffs", "forcecoefficients", "forcecoefficient", "aerodynamicloads", "aeroloads", "loads"),
+    "patch_flux": ("patchflowrate", "patchflow", "massflow", "massflux", "rhophi", "fluxhistory"),
+    "patch_pressure": ("patchaverage", "patchintegrate", "pressurerise", "pressuredifference", "patchpressure"),
+    "wall_law_profile": ("spaldingcomparison", "uplusyplus", "walllawprofile", "velocityprofile", "wallprofile"),
+    "centerline_profile": ("centerline", "centreline", "horizontal", "vertical", "px0", "py0", "rhox0", "rhoy0"),
+    "bubble_geometry": ("bubblegeometry", "bubblemetrics", "interfacegeometry"),
+}
+
+CONTRACT_VERSION = "foambench.evidence.contract.v1"
+CONTRACT_FILE = Path(__file__).resolve().parents[1] / "FoamBench_extended_openfoam13_evidence_contract.v1.json"
+
+# A manifest may use the QoI name instead of the routing kind.  This mapping
+# keeps that interface stable while allowing metric extractors to retain their
+# own physical validation rules.
+METRIC_KINDS = {
+    "Cd": "force_coefficients", "Cl": "force_coefficients", "Cm": "force_coefficients",
+    "Cd_mean": "force_coefficients", "Cd_rms": "force_coefficients",
+    "Cl_mean": "force_coefficients", "Cl_rms": "force_coefficients",
+    "first_cell_yplus": "wall_law_profile", "spalding_log_rmse": "wall_law_profile",
+    "centerline_profiles": "centerline_profile", "event_locations": "centerline_profile",
+    "mass_flow_rate": "patch_flux", "volumetric_flow_rate": "patch_flux",
+    "pressure_rise": "patch_pressure", "pressure_rise_history": "patch_pressure",
+}
+
+
+def compact_name(value: str) -> str:
+    return re.sub(r"[^a-z0-9]", "", value.lower())
+
+
+def evidence_roots(case: Path) -> tuple[Path, ...]:
+    parent = case.parent
+    roots = (
+        case / "postProcessing", case / "postprocessing", case / "results", case / "outputs",
+        parent / "postProcessing", parent / "postprocessing", parent / "results", parent / "outputs",
+        parent / "evidence", parent / "reports",
+    )
+    return tuple(dict.fromkeys(root for root in roots if root.is_dir()))
+
+
+def _manifest_paths(case: Path) -> tuple[Path, ...]:
+    """Locate the optional agent-emitted manifest without trusting its paths."""
+    return tuple(dict.fromkeys((case / "evidence/qoi_manifest.v1.json", case.parent / "evidence/qoi_manifest.v1.json")))
+
+
+def declared_evidence(case: Path, kind: str) -> list[Path]:
+    """Return manifest-declared files for *kind* after path containment checks."""
+    paths: list[Path] = []
+    accepted_metrics = {kind, *[metric for metric, mapped in METRIC_KINDS.items() if mapped == kind]}
+    for manifest_path in _manifest_paths(case):
+        try:
+            payload = json.loads(manifest_path.read_text(encoding="utf-8"))
+        except (OSError, ValueError, TypeError):
+            continue
+        entries = payload.get("entries", []) if isinstance(payload, dict) else []
+        if not isinstance(entries, list):
+            continue
+        for entry in entries:
+            if not isinstance(entry, dict) or entry.get("metric") not in accepted_metrics and entry.get("kind") != kind:
+                continue
+            raw = entry.get("path")
+            if not isinstance(raw, str) or not raw:
+                continue
+            candidate = (manifest_path.parent.parent / raw).resolve()
+            allowed = tuple(root.resolve() for root in evidence_roots(case))
+            if candidate.is_file() and any(candidate == root or root in candidate.parents for root in allowed):
+                paths.append(candidate)
+    return sorted(set(paths))
+
+
+def resolve_evidence(case: Path, kind: str, *, suffixes: tuple[str, ...] = ()) -> list[Path]:
+    """Return files whose path semantically addresses canonical evidence kind.
+
+    This function never parses or promotes a file.  The metric-specific
+    extractor remains responsible for schema/header/unit validation.
+    """
+    aliases = CANONICAL_ALIASES.get(kind, (kind,))
+    paths: set[Path] = set(declared_evidence(case, kind))
+    for root in evidence_roots(case):
+        for path in root.rglob("*"):
+            if not path.is_file():
+                continue
+            if suffixes and path.suffix.lower() not in suffixes:
+                continue
+            compact = compact_name(str(path))
+            if any(compact_name(alias) in compact for alias in aliases):
+                paths.add(path)
+    return sorted(paths)
+
+
+def canonical_evidence_manifest() -> dict[str, object]:
+    """Machine-readable resolver contract for reports and future agents."""
+    fallback = {
+        "schema_version": CONTRACT_VERSION,
+        "normalization": "lowercase_ascii_alphanumeric_path_matching",
+        "kinds": {key: list(value) for key, value in CANONICAL_ALIASES.items()},
+        "content_validation": "required_by_metric_extractor",
+        "proxy_policy": "semantic routing never authorizes a proxy metric",
+    }
+    try:
+        payload = json.loads(CONTRACT_FILE.read_text(encoding="utf-8"))
+    except (OSError, ValueError, TypeError):
+        return fallback
+    return payload if isinstance(payload, dict) else fallback
diff --git a/benchmarks/evaluation/execution.py b/benchmarks/evaluation/execution.py
new file mode 100644
index 0000000000000000000000000000000000000000..9d37479fa61904ccd51d3fd64dff75bae6bb89d3
--- /dev/null
+++ b/benchmarks/evaluation/execution.py
@@ -0,0 +1,62 @@
+from __future__ import annotations
+
+from typing import Any
+
+from .adapters.common import successful_formal_records
+from .foam import FATAL_RE, converged_early, final_log_time, latest_time_dir, normal_end, read_logs
+from .models import CaseArtifact
+
+
+def evaluate_execution(artifact: CaseArtifact, expected_time: float | None) -> dict[str, Any]:
+    case_dir = artifact.case_dir
+    latest, _ = latest_time_dir(case_dir)
+    logs = artifact.solver_logs
+    text = read_logs(logs)
+    log_time = final_log_time(text)
+    successful = successful_formal_records(artifact.formal_run_records)
+    requires_formal_record = (
+        artifact.workspace_dir is not None
+        and artifact.manifest.get("agent_mode") != "coding-only"
+        and artifact.manifest.get("domain_assets_enabled") is not False
+    )
+    manifest_status = str(artifact.manifest.get("status", ""))
+    timed_out = bool(artifact.manifest.get("timed_out")) or manifest_status == "timed_out"
+    process_ok = artifact.manifest.get("return_code") in {None, 0}
+    observed_time = max(value for value in (latest, log_time) if value is not None) if any(
+        value is not None for value in (latest, log_time)
+    ) else None
+    reached = observed_time is not None and (
+        expected_time is None
+        or observed_time >= expected_time - max(1e-12, abs(expected_time) * 1e-9)
+        or converged_early(text)
+    )
+    checks = {
+        "case_directory_exists": bool(case_dir and case_dir.is_dir()),
+        "control_dict_exists": bool(case_dir and (case_dir / "system" / "controlDict").is_file()),
+        "agent_not_timed_out": not timed_out,
+        "agent_process_succeeded": process_ok,
+        "formal_run_succeeded": bool(successful) if requires_formal_record else True,
+        "solver_log_exists": bool(logs),
+        "no_fatal_log_marker": FATAL_RE.search(text) is None,
+        "latest_time_exists": latest is not None,
+        "stop_condition_reached": reached,
+    }
+    # Some retained run records omit the literal OpenFOAM "End" line from the
+    # selected stdout ref. Keep it as evidence rather than a hard requirement.
+    evidence = {
+        "normal_end_marker": normal_end(text),
+        "converged_early_marker": converged_early(text),
+        "formal_run_records": [str(path) for path in successful],
+        "solver_logs": [str(path) for path in logs],
+    }
+    failed = [name for name, passed in checks.items() if not passed]
+    return {
+        "schema_version": "foambench.execution.v2",
+        "status": "pass" if not failed else "fail",
+        "expected_latest_time": expected_time,
+        "candidate_latest_time": latest,
+        "candidate_final_log_time": log_time,
+        "checks": checks,
+        "failed_checks": failed,
+        "evidence": evidence,
+    }
diff --git a/benchmarks/evaluation/extbench.py b/benchmarks/evaluation/extbench.py
new file mode 100644
index 0000000000000000000000000000000000000000..e3ebc3eab5f39bb77c676cce2b2a0b914013b6ef
--- /dev/null
+++ b/benchmarks/evaluation/extbench.py
@@ -0,0 +1,1572 @@
+#!/usr/bin/env python3
+"""Extract and audit Extended FoamBench QoIs without fallback proxies."""
+from __future__ import annotations
+
+import argparse
+import csv
+import json
+import math
+import re
+import statistics
+from pathlib import Path
+from typing import Any
+
+from .evidence_contract import canonical_evidence_manifest, evidence_roots, resolve_evidence
+from .foam_arrays import foam_path, read_label_list, read_scalar_field, read_vector_field, read_vector_list
+from .io import utc_now, write_json
+from .retained_fields import derive_cell_geometry, pump_measurements, static_mesh
+from .measurement_specs import load_measurement_spec
+
+ROOT = Path(__file__).resolve().parents[2]
+DEFAULT_DESIGN = ROOT / "benchmarks/FoamBench_extended_openfoam13_qoi_design.json"
+NUMERIC = re.compile(r"^[+-]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][+-]?\d+)?$")
+
+
+def named_numeric_rows(path: Path) -> tuple[list[str], list[list[float]]]:
+    """Read a whitespace/CSV table using the last compatible header."""
+    headers: list[list[str]] = []
+    rows: list[list[float]] = []
+    try:
+        for line in path.read_text(errors="ignore").splitlines():
+            stripped = line.strip()
+            if not stripped:
+                continue
+            if stripped.startswith("#"):
+                names = stripped[1:].strip().replace(",", " ").split()
+                if names:
+                    headers.append(names)
+                continue
+            parts = stripped.replace("(", " ").replace(")", " ").replace(",", " ").split()
+            if parts and all(NUMERIC.match(value) for value in parts):
+                rows.append([float(value) for value in parts])
+            elif (not rows and ("," in stripped or "\t" in stripped)
+                  and any(re.search(r"[A-Za-z_]", value) and not NUMERIC.fullmatch(value) for value in parts)):
+                names = [item.strip() for item in stripped.split(",")] if "," in stripped else stripped.split("\t")
+                if names:
+                    headers.append(names)
+    except OSError:
+        return [], []
+    if not rows:
+        return [], []
+    width = len(rows[0])
+    header = next((names for names in reversed(headers) if len(names) == width), [])
+    return header, [row for row in rows if len(row) == width]
+
+
+def matching_files(case: Path, needles: tuple[str, ...], suffixes: tuple[str, ...] = ()) -> list[Path]:
+    """Find explicit post-processing evidence in the case or its workspace."""
+    parent = case.parent
+    roots = [case / "postProcessing", case / "results", parent / "postProcessing", parent / "postprocessing", parent / "results"]
+    paths: list[Path] = []
+    for root in roots:
+        if not root.is_dir():
+            continue
+        paths.extend(path for path in root.rglob("*") if path.is_file()
+                     and (not suffixes or path.suffix.lower() in suffixes)
+                     and any(needle.lower() in str(path).lower() for needle in needles))
+    return sorted(set(paths))
+
+
+def evidence_path(case: Path, path: Path) -> str:
+    """Serialize evidence paths for both native case and sibling workspace outputs."""
+    try:
+        return str(path.relative_to(case))
+    except ValueError:
+        return "../" + str(path.relative_to(case.parent))
+
+
+def design_case_contract(case_id: str, design: dict[str, Any]) -> tuple[str | None, list[str]]:
+    """Return the branch and principal metrics for one family/variant."""
+    if "/" not in case_id:
+        raise ValueError(f"case id must be family/variant: {case_id}")
+    family_name, variant = case_id.split("/", 1)
+    family = next((item for item in design.get("families", []) if item.get("family") == family_name), None)
+    if family is None:
+        raise ValueError(f"design has no family for {case_id}")
+    return required_metrics(family, variant)
+
+
+def design_case_conditionals(case_id: str, design: dict[str, Any]) -> list[str]:
+    if "/" not in case_id:
+        raise ValueError(f"case id must be family/variant: {case_id}")
+    family_name, variant = case_id.split("/", 1)
+    family = next((item for item in design.get("families", []) if item.get("family") == family_name), None)
+    if family is None:
+        raise ValueError(f"design has no family for {case_id}")
+    for branch in family.get("branches", []):
+        if variant in branch.get("cases", []):
+            return [item["name"] for item in branch.get("conditional_qois", [])]
+    return []
+
+
+def extract_contract_case(case: Path, case_id: str, design: dict[str, Any] | None = None) -> dict[str, Any]:
+    """Extract one candidate using only the design contract."""
+    selected_design = design or json.loads(DEFAULT_DESIGN.read_text(encoding="utf-8"))
+    branch_id, metrics = design_case_contract(case_id, selected_design)
+    measurement_spec = load_measurement_spec(case_id)
+    if measurement_spec is not None:
+        declared = [item.get("metric") for item in measurement_spec.get("principal_measurements", [])]
+        if declared != metrics:
+            raise ValueError(f"measurement contract drift for {case_id}: {declared!r} != {metrics!r}")
+    conditionals = design_case_conditionals(case_id, selected_design)
+    result = extract_case(
+        case, case_id.split("/", 1)[0], case_id.split("/", 1)[1], metrics,
+        conditional_metrics=conditionals,
+    )
+    result["branch_id"] = branch_id
+    result["conditional_metrics"] = conditionals
+    result["contract_version"] = selected_design.get("schema_version")
+    if measurement_spec is not None:
+        result["measurement_contract"] = measurement_spec
+    return result
+
+
+def locate_case(run_root: Path, family: str, variant: str) -> Path | None:
+    candidates = (
+        run_root / f"{family}__{variant}" / "full_run_case",
+        run_root / f"{family}__{variant}" / "case",
+        run_root / family / variant / "full_run_case",
+        run_root / family / variant / "case",
+        run_root / family / variant,
+    )
+    return next((path for path in candidates if path.is_dir()), None)
+
+
+def required_metrics(family: dict[str, Any], variant: str) -> tuple[str | None, list[str]]:
+    for branch in family.get("branches", []):
+        if variant in branch.get("cases", []):
+            metrics = [item["name"] for item in branch.get("principal_qois", [])]
+            return branch.get("id"), metrics
+    return None, []
+
+
+def final_fraction(values: list[float], fraction: float = 0.2, minimum: int = 5) -> list[float]:
+    if not values:
+        return []
+    count = min(len(values), max(minimum, math.ceil(len(values) * fraction)))
+    return values[-count:]
+
+
+def force_coefficients(case: Path) -> tuple[dict[str, list[float]], list[str]]:
+    files = matching_files(case, ("forcecoeffs.dat",), (".dat", ".csv", ".raw"))
+    files.extend(resolve_evidence(case, "force_coefficients", suffixes=(".dat", ".csv", ".raw")))
+    # Content-addressed fallback: a different agent may call this table
+    # loads.csv or aero_coefficients.dat.  The header is the physical contract.
+    candidates = [path for root in evidence_roots(case) for path in root.rglob("*")
+                  if path.is_file() and path.suffix.lower() in {".dat", ".csv", ".raw"}]
+    for path in candidates:
+        if path in files:
+            continue
+        header, _ = named_numeric_rows(path)
+        if "Time" in header and any(name in header for name in ("Cd", "Cl", "Cm")):
+            files.append(path)
+    files = sorted(set(files))
+    columns: dict[str, list[float]] = {}
+    evidence: list[str] = []
+    for path in files:
+        header, rows = named_numeric_rows(path)
+        if not header or "Time" not in header:
+            continue
+        for name in ("Cd", "Cl", "Cm"):
+            if name not in header:
+                continue
+            index = header.index(name)
+            columns.setdefault(name, []).extend(
+                row[index] for row in rows if math.isfinite(row[index])
+            )
+        evidence.append(evidence_path(case, path))
+    return columns, evidence
+
+
+def extract_force_metric(case: Path, metric: str) -> tuple[float | None, list[str], str]:
+    columns, evidence = force_coefficients(case)
+    base = metric.removesuffix("_mean").removesuffix("_rms")
+    values = final_fraction(columns.get(base, []))
+    if not values:
+        return None, [], "header_addressed_force_coefficients.v1"
+    if metric.endswith("_rms"):
+        mean = statistics.fmean(values)
+        value = math.sqrt(statistics.fmean((item - mean) ** 2 for item in values))
+    else:
+        value = statistics.fmean(values)
+    return value, evidence, "header_addressed_force_coefficients.v1"
+
+
+def spalding_metrics_from_files(files: list[Path], relative_to: Path) -> tuple[dict[str, float], list[str]]:
+    log_errors: list[float] = []
+    first_yplus: list[float] = []
+    evidence: list[str] = []
+    for path in files:
+        header, rows = named_numeric_rows(path)
+        normalized = {
+            re.sub(r"[^a-z0-9]", "", name.lower().replace("+", "plus")): index
+            for index, name in enumerate(header)
+        }
+        y_index = next(
+            (normalized[name] for name in ("yplus", "firstcellyplus", "yplusmin", "firstcellyplusmin") if name in normalized),
+            None,
+        )
+        predicted_index = next(
+            (normalized[name] for name in ("spaldingyplus", "yplusspaldingup", "yplusspaldinguplus", "yplusspalding") if name in normalized),
+            None,
+        )
+        if y_index is None:
+            continue
+        # Zero is a valid observed wall resolution.  Missing evidence is an
+        # absent row, not a non-positive value.
+        y_values = [row[y_index] for row in rows if len(row) > y_index and math.isfinite(row[y_index]) and row[y_index] >= 0]
+        if y_values:
+            first_yplus.append(min(y_values))
+        if predicted_index is None:
+            # A first-cell summary is valid endpoint evidence, but it cannot
+            # be relabelled as a profile residual.
+            evidence.append(evidence_path(relative_to, path))
+            continue
+        valid = [
+            (row[y_index], row[predicted_index]) for row in rows
+            if len(row) > max(y_index, predicted_index)
+            and math.isfinite(row[y_index]) and math.isfinite(row[predicted_index])
+            and row[y_index] >= 0 and row[predicted_index] >= 0
+        ]
+        if not valid:
+            continue
+        log_errors.extend(
+            math.log1p(yplus) - math.log1p(predicted)
+            for yplus, predicted in valid
+        )
+        evidence.append(evidence_path(relative_to, path))
+    result: dict[str, float] = {}
+    if log_errors:
+        result["spalding_log_rmse"] = math.sqrt(statistics.fmean(value * value for value in log_errors))
+    if first_yplus:
+        result["first_cell_yplus"] = statistics.fmean(first_yplus)
+    return result, evidence
+
+
+def standard_yplus_metrics(files: list[Path], relative_to: Path) -> tuple[dict[str, float], list[str]]:
+    """Read OpenFOAM's standard ``yPlus.dat`` patch summary.
+
+    The standard table has the schema ``Time patch min max average``.  It is
+    therefore intentionally parsed separately from ``named_numeric_rows``,
+    which rejects the non-numeric patch column.  A zero average remains a
+    valid observation.
+    """
+    rows: list[tuple[float, str, float, float, float]] = []
+    evidence: list[str] = []
+    for path in files:
+        if path.name.lower() != "yplus.dat":
+            continue
+        try:
+            for line in path.read_text(encoding="utf-8", errors="ignore").splitlines():
+                parts = line.split()
+                if len(parts) < 5 or parts[0].startswith("#"):
+                    continue
+                try:
+                    time = float(parts[0])
+                    minimum, maximum, average = float(parts[2]), float(parts[3]), float(parts[4])
+                except ValueError:
+                    continue
+                if all(math.isfinite(value) for value in (time, minimum, maximum, average)):
+                    rows.append((time, parts[1], minimum, maximum, average))
+        except OSError:
+            continue
+        if rows:
+            evidence.append(evidence_path(relative_to, path))
+    if not rows:
+        return {}, []
+    final_time = max(row[0] for row in rows)
+    final_rows = [row for row in rows if abs(row[0] - final_time) <= 1e-12 * max(1.0, abs(final_time))]
+    # Symmetric wall patches are one declared response; average their final
+    # values while retaining the source file as auditable evidence.
+    return {"first_cell_yplus": statistics.fmean(row[4] for row in final_rows)}, sorted(set(evidence))
+
+
+def spalding_metrics(case: Path) -> tuple[dict[str, float], list[str]]:
+    files = matching_files(case, ("spalding_comparison", "uplus_yplus", "wall_law_profile"), (".raw", ".xy", ".dat", ".csv"))
+    # OpenFOAM's standard yPlus function object writes ``yPlus.dat`` with a
+    # non-numeric patch-name column (``Time patch min max average``).  It is
+    # intentionally handled by ``standard_yplus_metrics`` below, so discover
+    # it by basename instead of sending it through ``named_numeric_rows``.
+    for root in evidence_roots(case):
+        files.extend(
+            path for path in root.rglob("*")
+            if path.is_file() and path.name.lower() == "yplus.dat"
+        )
+    # The rollout measurement writer emits an explicit wall table instead of
+    # a Spalding profile.  yPlus_min is valid endpoint evidence; it is not
+    # treated as a profile residual.
+    files.extend(matching_files(case, ("yplus_wall.csv",), (".csv",)))
+    # Accept semantically equivalent wall tables even when the file name is
+    # agent-specific, provided the table contains a y+ column.
+    for root in evidence_roots(case):
+        for path in root.rglob("*"):
+            if not path.is_file() or path.suffix.lower() not in {".csv", ".dat", ".raw", ".xy"}:
+                continue
+            header, _ = named_numeric_rows(path)
+            normalized = {re.sub(r"[^a-z0-9]", "", name.lower().replace("+", "plus")) for name in header}
+            if "yplus" in normalized or "firstcellyplus" in normalized:
+                files.append(path)
+    files = sorted(set(files))
+    standard_values, standard_evidence = standard_yplus_metrics(files, case)
+    wall_files = [path for path in files if path.name.lower() == "yplus_wall.csv"]
+    wall_values: list[float] = []
+    wall_evidence: list[str] = []
+    for path in wall_files:
+        try:
+            with path.open(newline="", encoding="utf-8", errors="ignore") as handle:
+                for row in csv.DictReader(handle):
+                    raw = row.get("yPlus_min") or row.get("yplus_min") or row.get("first_cell_yplus")
+                    if raw is not None:
+                        value = float(raw)
+                        if math.isfinite(value) and value >= 0:
+                            wall_values.append(value)
+                if wall_values:
+                    wall_evidence.append(evidence_path(case, path))
+        except (OSError, ValueError):
+            continue
+    # Branch-labelled evidence is handled separately for the multi-Re case.
+    files = [path for path in files if "branches" not in tuple(evidence_path(case, path).split("/"))]
+    values, evidence = spalding_metrics_from_files([path for path in files if path not in wall_files], case)
+    if "first_cell_yplus" not in values:
+        # CSV profile variants use a header with a literal ``y+`` token or a
+        # yplus column and do not necessarily contain a yPlus_min summary.
+        for path in files:
+            if path in wall_files:
+                continue
+            header, rows = named_numeric_rows(path)
+            normalized = {re.sub(r"[^a-z0-9]", "", name.lower().replace("+", "plus")): i for i, name in enumerate(header)}
+            index = next((normalized[name] for name in ("yplus", "firstcellyplus") if name in normalized), None)
+            if index is not None:
+                vals = [row[index] for row in rows if len(row) > index and math.isfinite(row[index]) and row[index] >= 0]
+                if vals:
+                    values["first_cell_yplus"] = vals[0]
+                    evidence.append(evidence_path(case, path))
+                    break
+    if wall_values:
+        # The final row is the retained endpoint; using the mean would mix
+        # initialization transients with the declared final wall resolution.
+        values["first_cell_yplus"] = wall_values[-1]
+        evidence.extend(wall_evidence)
+    if "first_cell_yplus" not in values and standard_values:
+        values.update(standard_values)
+        evidence.extend(standard_evidence)
+    return values, sorted(set(evidence))
+
+
+def branchwise_spalding_metrics(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    branches: dict[str, Any] = {}
+    evidence: list[str] = []
+    files = matching_files(case, ("spalding_comparison", "uplus_yplus", "wall_law_profile"), (".raw", ".xy", ".dat", ".csv"))
+    by_branch: dict[str, list[Path]] = {}
+    for path in files:
+        match = re.search(r"Re_tau_(180|395|590)", str(path))
+        if match:
+            by_branch.setdefault(f"Re_tau_{match.group(1)}", []).append(path)
+    for branch, branch_files in sorted(by_branch.items()):
+        values, refs = spalding_metrics_from_files(sorted(branch_files), case)
+        if {"spalding_log_rmse", "first_cell_yplus"} <= set(values):
+            branches[branch] = values
+            evidence.extend(refs)
+    expected = {"Re_tau_180", "Re_tau_395", "Re_tau_590"}
+    if set(branches) != expected:
+        return None, sorted(set(evidence))
+    return {"kind": "branch_scalars", "branches": branches}, sorted(set(evidence))
+
+
+def stirrer_power_history(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    files = matching_files(case, ("surfaceFieldValue.dat",), (".dat",))
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    for path in files:
+        header, rows = named_numeric_rows(path)
+        fields = [name for name in header if name != "Time" and "stressUSf" in name]
+        if "Time" not in header or not fields:
+            continue
+        time_index, power_index = header.index("Time"), header.index(fields[0])
+        points.extend({"time": row[time_index], "value": row[power_index]} for row in rows if math.isfinite(row[power_index]))
+        evidence.append(evidence_path(case, path))
+    if not points:
+        return None, []
+    points.sort(key=lambda item: item["time"])
+    return {"kind": "time_history", "quantity": "surface_integrated_stressUSf_power", "points": points}, evidence
+
+
+def named_sample_profiles(case: Path, names: tuple[str, ...]) -> tuple[dict[str, Any] | None, list[str]]:
+    profiles: list[dict[str, Any]] = []
+    evidence: list[str] = []
+    roots = [case, *evidence_roots(case)]
+    candidates: list[Path] = []
+    for root in roots:
+        candidates.extend(item for item in root.rglob("*") if item.is_file() and (
+            item.name in names or (item.suffix.lower() == ".csv" and item.parent.name.lower() == "profiles")
+        ))
+    for path in sorted(set(candidates)):
+        header, rows = named_numeric_rows(path)
+        if len(header) < 2 or not rows or not profile_has_physical_columns(header):
+            continue
+        profiles.append({
+            "profile_id": evidence_path(case, path),
+            "columns": header,
+            "rows": rows,
+        })
+        evidence.append(evidence_path(case, path))
+    if not profiles:
+        return None, []
+    return {"kind": "named_profiles", "profiles": profiles}, evidence
+
+
+def result_profile_tables(case: Path, tokens: tuple[str, ...]) -> tuple[dict[str, Any] | None, list[str]]:
+    """Read explicit profile tables from workspace/results when named output
+    files use a family-specific filename instead of horizontal.xy/vertical.xy.
+    """
+    profiles: list[dict[str, Any]] = []
+    evidence: list[str] = []
+    roots = list(evidence_roots(case))
+    resolved = resolve_evidence(case, "centerline_profile", suffixes=(".csv", ".dat", ".raw", ".xy"))
+    for root in roots:
+        if not root.is_dir():
+            continue
+        for path in sorted(root.rglob("*")):
+            if not path.is_file() or path.suffix.lower() not in {".csv", ".dat", ".raw", ".xy"}:
+                continue
+            if path not in resolved and not any(token.lower() in path.name.lower() for token in tokens):
+                continue
+            header, rows = named_numeric_rows(path)
+            if len(header) < 2 or not rows or not profile_has_physical_columns(header):
+                continue
+            profiles.append({"profile_id": evidence_path(case, path), "columns": header, "rows": rows})
+            evidence.append(evidence_path(case, path))
+    if not profiles:
+        return None, []
+    return {"kind": "named_profiles", "profiles": profiles}, sorted(set(evidence))
+
+
+def profile_has_physical_columns(header: list[str]) -> bool:
+    """Require a coordinate and at least one sampled physical field."""
+    normalized = [re.sub(r"[^a-z0-9]", "", name.lower()) for name in header]
+    has_coordinate = any(name in {"x", "y", "z", "coordinate", "position", "arc"} or name.startswith(("x", "y", "z")) for name in normalized)
+    has_field = any(
+        name in {"p", "rho", "u", "ux", "uy", "uz"}
+        or name.startswith(("px", "py", "pz", "rhox", "rhoy", "rhoz"))
+        for name in normalized
+    )
+    return has_coordinate and has_field
+
+
+def named_profiles_containing(case: Path, tokens: tuple[str, ...], required_columns: tuple[str, ...] = ()) -> tuple[dict[str, Any] | None, list[str]]:
+    """Read explicitly named sample tables; never infer a physical metric from field extrema."""
+    profiles: list[dict[str, Any]] = []
+    evidence: list[str] = []
+    for root in (case, *evidence_roots(case)):
+        for path in sorted(item for item in root.rglob("*") if item.is_file() and path_like_sample(item, tokens)):
+            header, rows = named_numeric_rows(path)
+            if len(header) < 2 or not rows or any(column not in header for column in required_columns):
+                continue
+            profiles.append({"profile_id": evidence_path(case, path), "columns": header, "rows": rows})
+            evidence.append(evidence_path(case, path))
+    return ({"kind": "named_profiles", "profiles": profiles}, evidence) if profiles else (None, [])
+
+
+def path_like_sample(path: Path, tokens: tuple[str, ...]) -> bool:
+    name = path.name.lower()
+    return path.suffix.lower() in {".xy", ".raw", ".dat", ".csv"} and any(token.lower() in name for token in tokens)
+
+
+def field_dimensions(case: Path, field: str) -> str | None:
+    for path in sorted(case.rglob(field), reverse=True):
+        if not path.is_file() or not path.parent.name.replace(".", "", 1).isdigit():
+            continue
+        header = path.read_bytes()[:4096].decode("ascii", errors="ignore")
+        match = re.search(r"dimensions\s*\[([^]]+)\]", header)
+        if match:
+            return " ".join(match.group(1).split())
+    return None
+
+
+def evidence_branch(case: Path, path: Path) -> str:
+    try:
+        parts = path.relative_to(case).parts
+    except ValueError:
+        parts = path.relative_to(case.parent).parts
+    try:
+        index = parts.index("postProcessing")
+    except ValueError:
+        return "root"
+    return "/".join(parts[:index]) or "root"
+
+
+def explicit_mass_flow_history(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    branch_points: dict[str, list[dict[str, float]]] = {}
+    evidence: list[str] = []
+    candidates = matching_files(case, ("surfaceFieldValue", "massFlow", "massFlux", "rhoPhi"), (".dat", ".raw", ".csv"))
+    # Some benchmark variants materialize several nested operating-point cases;
+    # accept their postProcessing evidence without flattening those branches.
+    if not candidates:
+        candidates = sorted(path for path in case.rglob("*") if path.is_file()
+                            and path.suffix.lower() in {".dat", ".raw", ".csv"}
+                            and any(token.lower() in str(path).lower()
+                                    for token in ("surfaceFieldValue", "massFlow", "massFlux", "rhoPhi")))
+    for path in candidates:
+        patch_match = re.search(r"patch=([^)/]+)", str(path))
+        if patch_match is not None and patch_match.group(1).lower() not in {"inlet", "inlet1", "main", "mainstream"}:
+            # The principal pump/nozzle response is the declared inlet flow;
+            # do not concatenate inlet and outlet fluxes into one history.
+            continue
+        header, rows = named_numeric_rows(path)
+        mass_columns = [column for column in header if any(token in column.lower() for token in ("rhophi", "massflow", "massflux", "sum(phi)"))]
+        if "Time" not in header or not mass_columns:
+            continue
+        t_index, value_index = header.index("Time"), header.index(mass_columns[0])
+        branch = evidence_branch(case, path)
+        branch_points.setdefault(branch, []).extend(
+            {"time": row[t_index], "value": row[value_index]}
+            for row in rows if math.isfinite(row[value_index])
+        )
+        evidence.append(evidence_path(case, path))
+    if not branch_points:
+        return None, []
+    dimensions = field_dimensions(case, "phi")
+    quantity = {
+        "1 0 -1 0 0 0 0": "explicit_mass_flow",
+        "0 3 -1 0 0 0 0": "explicit_volumetric_flow",
+    }.get(dimensions, "explicit_flux_unknown_dimensions")
+    branches = {
+        branch: {"kind": "time_history", "quantity": quantity,
+                 "points": sorted(points, key=lambda item: item["time"])}
+        for branch, points in sorted(branch_points.items())
+    }
+    if set(branches) == {"root"}:
+        result = branches["root"]
+    else:
+        result = {"kind": "branched_time_histories", "quantity": quantity, "branches": branches}
+    result["field_dimensions"] = dimensions
+    return result, sorted(set(evidence))
+
+
+def explicit_patch_pressure(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    histories: dict[str, list[dict[str, float]]] = {}
+    evidence: list[str] = []
+    for path in matching_files(case, ("patchAverage", "patchIntegrate", "pressureRise", "pressure_rise"), (".dat", ".raw", ".csv")):
+        header, rows = named_numeric_rows(path)
+        pressure_columns = [column for column in header if column != "Time" and any(token in column.lower() for token in ("p", "pressure"))]
+        match = re.search(r"patch=([^)/]+)", str(path))
+        if "Time" not in header or not pressure_columns or not match:
+            continue
+        patch_name = match.group(1)
+        t_index, value_index = header.index("Time"), header.index(pressure_columns[0])
+        histories.setdefault(patch_name, []).extend({"time": row[t_index], "value": row[value_index]} for row in rows if math.isfinite(row[value_index]))
+        evidence.append(evidence_path(case, path))
+    inlet_name = next((name for name in histories if "inlet" in name.lower()), None)
+    outlet_name = next((name for name in histories if "outlet" in name.lower()), None)
+    if inlet_name is None or outlet_name is None:
+        return None, []
+    inlet = {round(point["time"], 12): point["value"] for point in histories[inlet_name]}
+    outlet = {round(point["time"], 12): point["value"] for point in histories[outlet_name]}
+    points = [
+        {"time": time, "value": outlet[time] - inlet[time]}
+        for time in sorted(set(inlet) & set(outlet))
+    ]
+    if not points:
+        return None, []
+    return {
+        "kind": "time_history",
+        "quantity": "pressure_rise",
+        "definition": "outlet_minus_inlet_patch_average",
+        "source_patches": {"inlet": inlet_name, "outlet": outlet_name},
+        "points": points,
+    }, sorted(set(evidence))
+
+
+def crossjet_inlet_mass_flux_ratio(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    fluxes: dict[str, list[tuple[float, float]]] = {}
+    evidence: list[str] = []
+    for path in resolve_evidence(case, "patch_flux", suffixes=(".dat", ".raw", ".csv")):
+        match = re.search(r"patch=([^)/]+)", str(path))
+        if match is None:
+            match = re.search(r"(?m)^\s*#\s*Selection\s*:\s*patch\(([^)]+)\)", path.read_text(errors="ignore"))
+        if match is None:
+            continue
+        patch = match.group(1).lower()
+        canonical = (
+            "inlet1" if patch in {"inlet1", "inlet", "main", "mainstream", "maininlet", "mainflowinlet"}
+            else "inlet2" if patch in {"inlet2", "jet", "injection", "jetinlet"}
+            else None
+        )
+        if canonical is None:
+            continue
+        header, rows = named_numeric_rows(path)
+        columns = [column for column in header if column != "Time" and "sum(phi)" in column]
+        if "Time" not in header or not columns:
+            continue
+        ti, vi = header.index("Time"), header.index(columns[0])
+        fluxes.setdefault(canonical, []).extend((row[ti], row[vi]) for row in rows)
+        evidence.append(evidence_path(case, path))
+    if not all(fluxes.get(patch) for patch in ("inlet1", "inlet2")):
+        return None, []
+    main = sorted(fluxes["inlet1"])[-1]
+    jet = sorted(fluxes["inlet2"])[-1]
+    if main[1] == 0:
+        return None, []
+    return {
+        "kind": "scalar_ratio",
+        "quantity": "jet_to_mainstream_mass_flux_ratio",
+        "value": abs(jet[1] / main[1]),
+        "mainstream_flux": main[1],
+        "jet_flux": jet[1],
+        "time": min(main[0], jet[0]),
+        "patch_aliases": {"mainstream": "inlet1", "jet": "inlet2"},
+    }, sorted(set(evidence))
+
+
+def phase_volume_history(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    for time, directory in numeric_time_dirs(case):
+        alpha_path = foam_path(directory, "alpha.water")
+        volume_path = foam_path(directory, "Vc")
+        if alpha_path is None or volume_path is None:
+            continue
+        try:
+            alpha = read_scalar_field(alpha_path)
+            volumes = read_scalar_field(volume_path)
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(alpha) != len(volumes) or not volumes:
+            continue
+        total = sum(volumes)
+        if total <= 0:
+            continue
+        points.append({"time": time, "value": sum(a * v for a, v in zip(alpha, volumes)) / total})
+        evidence.extend((evidence_path(case, alpha_path), evidence_path(case, volume_path)))
+    if not points:
+        return None, []
+    return {"kind": "time_history", "quantity": "volume_weighted_alpha_water", "points": points}, sorted(set(evidence))
+
+
+def volume_average_speed_history(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    for time, directory in numeric_time_dirs(case):
+        velocity_path = foam_path(directory, "U")
+        volume_path = foam_path(directory, "Vc")
+        if velocity_path is None or volume_path is None:
+            continue
+        try:
+            velocity = read_vector_field(velocity_path)
+            volumes = read_scalar_field(volume_path)
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(velocity) != len(volumes) or not volumes:
+            continue
+        total = sum(volumes)
+        if total <= 0:
+            continue
+        value = sum(math.sqrt(u * u + v * v + w * w) * volume
+                    for (u, v, w), volume in zip(velocity, volumes)) / total
+        if not math.isfinite(value):
+            continue
+        points.append({"time": time, "value": value})
+        evidence.extend((evidence_path(case, velocity_path), evidence_path(case, volume_path)))
+    if not points:
+        return None, []
+    return {"kind": "time_history", "quantity": "volume_average_speed", "points": points}, sorted(set(evidence))
+
+
+def volume_speed_rms_history(case: Path) -> tuple[dict[str, Any] | None, list[str]]:
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    for time, directory in numeric_time_dirs(case):
+        velocity_path, volume_path = foam_path(directory, "U"), foam_path(directory, "Vc")
+        if velocity_path is None or volume_path is None:
+            continue
+        try:
+            velocity, volumes = read_vector_field(velocity_path), read_scalar_field(volume_path)
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(velocity) != len(volumes) or not volumes or sum(volumes) <= 0:
+            continue
+        speeds = [math.sqrt(u * u + v * v + w * w) for u, v, w in velocity]
+        total = sum(volumes)
+        mean = sum(speed * volume for speed, volume in zip(speeds, volumes)) / total
+        rms = math.sqrt(sum((speed - mean) ** 2 * volume for speed, volume in zip(speeds, volumes)) / total)
+        if math.isfinite(rms):
+            points.append({"time": time, "value": rms})
+            evidence.extend((evidence_path(case, velocity_path), evidence_path(case, volume_path)))
+    if not points:
+        return None, []
+    return {"kind": "time_history", "quantity": "volume_speed_spatial_rms", "points": points}, sorted(set(evidence))
+
+
+def volume_average_speed_final(case: Path) -> tuple[float | None, list[str]]:
+    """Extract a final-state mixing response from retained U and cell volumes."""
+    for _, directory in reversed(numeric_time_dirs(case)):
+        velocity_path, volume_path = foam_path(directory, "U"), foam_path(directory, "Vc")
+        if velocity_path is None:
+            continue
+        try:
+            # Retained agent fields can contain a uniform internal U while Vc
+            # still has one volume per cell.  Decode the concrete array first
+            # so the uniform vector is expanded using an observed cell count.
+            if volume_path is not None:
+                volumes = read_scalar_field(volume_path)
+                geometry_evidence = [volume_path]
+            else:
+                from .retained_fields import derive_cell_geometry
+                volumes, _, geometry_evidence = derive_cell_geometry(case)
+            try:
+                velocity = read_vector_field(velocity_path)
+            except (ValueError, RuntimeError):
+                velocity = read_vector_field_allow_uniform(velocity_path, len(volumes))
+            if volume_path is not None and len(volumes) == 1 and len(velocity) > 1:
+                volumes = volumes * len(velocity)
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(velocity) != len(volumes) or not volumes or sum(volumes) <= 0:
+            continue
+        total = sum(volumes)
+        value = sum(math.sqrt(u * u + v * v + w * w) * volume
+                    for (u, v, w), volume in zip(velocity, volumes)) / total
+        if math.isfinite(value):
+            return value, [evidence_path(case, path) for path in [velocity_path, *geometry_evidence]]
+    return None, []
+
+
+def read_vector_field_allow_uniform(path: Path, count: int) -> list[tuple[float, float, float]]:
+    try:
+        return read_vector_field(path)
+    except (ValueError, RuntimeError):
+        text = path.read_text(encoding="ascii", errors="ignore")
+        match = re.search(r"internalField\s+uniform\s+\(([^)]+)\)", text)
+        if match is None:
+            raise
+        values = [float(item) for item in match.group(1).split()]
+        if len(values) != 3:
+            raise ValueError(f"invalid uniform vector field: {path}")
+        return [(values[0], values[1], values[2])] * count
+
+
+def read_scalar_field_allow_uniform(path: Path, count: int) -> list[float]:
+    """Read a scalar field while preserving the semantics of a uniform field."""
+    try:
+        values = read_scalar_field(path)
+    except (ValueError, RuntimeError):
+        text = path.read_text(encoding="ascii", errors="ignore")
+        match = re.search(r"internalField\s+uniform\s+([^;]+);", text)
+        if match is None:
+            raise
+        return [float(match.group(1).strip())] * count
+    if len(values) == 1 and count > 1:
+        # OpenFOAM permits a uniform field to be serialized as one value.
+        return values * count
+    return values
+
+
+def crossjet_interior_pressure_span(case: Path) -> tuple[float | None, list[str]]:
+    """Return the pressure response in the declared internal CrossJet window.
+
+    The span is deliberately computed from the retained pressure field rather
+    than from ``grad(p)``.  This remains extractable for references that store
+    ``p`` as a uniform field and avoids treating a missing/zero post-processing
+    gradient as a shock observable.
+    """
+    for _, directory in reversed(numeric_time_dirs(case)):
+        centre_path, pressure_path = foam_path(directory, "C"), foam_path(directory, "p")
+        if pressure_path is None:
+            continue
+        try:
+            if centre_path is not None:
+                centres = read_vector_field(centre_path)
+                geometry_evidence = [centre_path]
+            else:
+                from .retained_fields import derive_cell_geometry
+                _, centres, geometry_evidence = derive_cell_geometry(case)
+            pressure = read_scalar_field_allow_uniform(pressure_path, len(centres))
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(pressure) != len(centres):
+            continue
+        values = [value for (x, y, _), value in zip(centres, pressure)
+                  if -1.0 <= x <= 1.0 and 0.1 <= y <= 0.95]
+        if values:
+            return max(values) - min(values), [evidence_path(case, path) for path in [*geometry_evidence, pressure_path]]
+    return None, []
+
+
+def crossjet_interior_pressure_gradient_max(case: Path) -> tuple[float | None, list[str]]:
+    """Return the maximum interior pressure span."""
+    return crossjet_interior_pressure_span(case)
+
+
+def profile_event_locations(profiles: dict[str, Any]) -> dict[str, Any] | None:
+    events: list[dict[str, Any]] = []
+    for profile in profiles.get("profiles", []):
+        columns = profile.get("columns", [])
+        rows = profile.get("rows", [])
+        if len(columns) < 2 or len(rows) < 5:
+            continue
+        coordinate_index = 0
+        for field in ("p", "rho"):
+            field_index = next((index for index, name in enumerate(columns)
+                                if name.lower() == field or name.lower().startswith(field + "_")), None)
+            if field_index is None:
+                continue
+            gradients: list[tuple[int, float, float]] = []
+            for index in range(len(rows) - 1):
+                spacing = abs(rows[index + 1][coordinate_index] - rows[index][coordinate_index])
+                if spacing <= 0:
+                    continue
+                gradient = abs(rows[index + 1][field_index] - rows[index][field_index]) / spacing
+                coordinate = (rows[index + 1][coordinate_index] + rows[index][coordinate_index]) / 2
+                gradients.append((index, coordinate, gradient))
+            if not gradients:
+                continue
+            peak = max(value for _, _, value in gradients)
+            threshold = 0.05 * peak
+            candidates = [
+                item for position, item in enumerate(gradients)
+                if item[2] >= threshold
+                and (position == 0 or item[2] >= gradients[position - 1][2])
+                and (position == len(gradients) - 1 or item[2] > gradients[position + 1][2])
+            ]
+            selected: list[tuple[int, float, float]] = []
+            for candidate in sorted(candidates, key=lambda item: item[2], reverse=True):
+                if all(abs(candidate[0] - item[0]) >= 4 for item in selected):
+                    selected.append(candidate)
+                if len(selected) == 12:
+                    break
+            for index, coordinate, magnitude in sorted(selected, key=lambda item: item[1]):
+                local_spacing = abs(rows[index + 1][coordinate_index] - rows[index][coordinate_index])
+                events.append({
+                    "profile_id": profile["profile_id"],
+                    "field": field,
+                    "coordinate": coordinate,
+                    "gradient_magnitude": magnitude,
+                    "local_cell_size": local_spacing,
+                })
+    if not events:
+        return None
+    return {
+        "kind": "profile_feature_locations",
+        "detector": "local_abs_gradient_peaks.v1",
+        "relative_prominence": 0.05,
+        "minimum_separation_samples": 4,
+        "maximum_features_per_field_profile": 12,
+        "events": events,
+    }
+
+
+def final_riemann_profiles(profiles: dict[str, Any]) -> dict[str, Any]:
+    """Select each centerline's latest saved time and use its physical axis.
+
+    OpenFOAM raw sets may prefix x/y/z with arc distance. Preserve the sampled
+    values, but put x (horizontal) or y (vertical) first for event detection.
+    """
+    from .comparison import profile_key
+    selected: dict[str, tuple[float, dict[str, Any]]] = {}
+    for profile in profiles.get("profiles", []):
+        key = profile_key(profile)
+        axis = {"horizontal.xy": "x", "vertical.xy": "y"}.get(key)
+        columns = profile.get("columns", [])
+        if axis is None or axis not in columns:
+            continue
+        try:
+            time = float(Path(profile["profile_id"]).parent.name)
+        except ValueError:
+            time = -math.inf
+        if key in selected and time < selected[key][0]:
+            continue
+        order = [columns.index(axis)] + [i for i, name in enumerate(columns) if name != axis]
+        normalized = {**profile, "columns": [columns[i] for i in order],
+                      "rows": [[row[i] for i in order] for row in profile["rows"]]}
+        selected[key] = (time, normalized)
+    return {"kind": "named_profiles", "profiles": [item[1] for item in selected.values()]}
+
+
+def numeric_time_dirs(case: Path) -> list[tuple[float, Path]]:
+    result: list[tuple[float, Path]] = []
+    for path in case.iterdir():
+        if not path.is_dir():
+            continue
+        try:
+            result.append((float(path.name), path))
+        except ValueError:
+            pass
+    return sorted(result)
+
+
+def mesh_dir(case: Path, time_dir: Path) -> Path:
+    local = time_dir / "polyMesh"
+    return local if local.is_dir() else case / "constant/polyMesh"
+
+
+def connected_components(active: set[int], owner: list[int], neighbour: list[int]) -> list[list[int]]:
+    adjacency: dict[int, list[int]] = {cell: [] for cell in active}
+    for left, right in zip(owner, neighbour):
+        if left in active and right in active:
+            adjacency[left].append(right)
+            adjacency[right].append(left)
+    components: list[list[int]] = []
+    unseen = set(active)
+    while unseen:
+        seed = unseen.pop()
+        stack = [seed]
+        component = [seed]
+        while stack:
+            for cell in adjacency[stack.pop()]:
+                if cell in unseen:
+                    unseen.remove(cell)
+                    stack.append(cell)
+                    component.append(cell)
+        components.append(component)
+    return components
+
+
+def component_geometry(
+    cells: list[int], gas: list[float], volumes: list[float], centres: list[tuple[float, float, float]], volume_factor: float
+) -> dict[str, float]:
+    weights = [max(0.0, min(1.0, gas[cell])) * volumes[cell] for cell in cells]
+    volume = sum(weights)
+    if volume <= 0:
+        return {}
+    centroid = [sum(weight * centres[cell][axis] for weight, cell in zip(weights, cells)) / volume for axis in range(3)]
+    xx = sum(weight * (centres[cell][0] - centroid[0]) ** 2 for weight, cell in zip(weights, cells)) / volume
+    yy = sum(weight * (centres[cell][1] - centroid[1]) ** 2 for weight, cell in zip(weights, cells)) / volume
+    xy = sum(weight * (centres[cell][0] - centroid[0]) * (centres[cell][1] - centroid[1]) for weight, cell in zip(weights, cells)) / volume
+    root = math.sqrt(max(0.0, (xx - yy) ** 2 + 4 * xy * xy))
+    major = max(0.0, (xx + yy + root) / 2)
+    minor = max(0.0, (xx + yy - root) / 2)
+    aspect = math.sqrt(major / minor) if minor > 0 else None
+    return {
+        "volume": volume,
+        "centroid_x": centroid[0],
+        "centroid_y": centroid[1],
+        "centroid_z": centroid[2],
+        "aspect_ratio": aspect,
+        "equivalent_radius_3d": (3 * volume * volume_factor / (4 * math.pi)) ** (1 / 3),
+    }
+
+
+def axisymmetric_volume_factor(case: Path) -> float:
+    boundary = case / "constant/polyMesh/boundary"
+    if not boundary.is_file() or "wedge" not in boundary.read_text(encoding="utf-8", errors="ignore"):
+        return 1.0
+    points_path = foam_path(case / "constant/polyMesh", "points")
+    if points_path is None:
+        return 1.0
+    angles = [math.atan2(y, x) for x, y, _ in read_vector_list(points_path) if x > 0]
+    if not angles:
+        return 1.0
+    wedge_angle = max(angles) - min(angles)
+    return 2 * math.pi / wedge_angle if wedge_angle > 0 else 1.0
+
+
+def bubble_history(case: Path) -> tuple[list[dict[str, Any]], list[str], list[str]]:
+    history: list[dict[str, Any]] = []
+    evidence: list[str] = []
+    errors: list[str] = []
+    dynamic = not static_mesh(case)
+    volume_factor = axisymmetric_volume_factor(case)
+    cached_geometry: tuple[list[float], list[tuple[float, float, float]]] | None = None
+    cached_topology: tuple[list[int], list[int]] | None = None
+    time_dirs = numeric_time_dirs(case)
+    if not dynamic:
+        for _, directory in reversed(time_dirs):
+            volume_path = foam_path(directory, "Vc")
+            centre_path = foam_path(directory, "C")
+            if volume_path and centre_path:
+                cached_geometry = (read_scalar_field(volume_path), read_vector_field(centre_path))
+                break
+        topology_dir = case / "constant/polyMesh"
+        owner_path = foam_path(topology_dir, "owner")
+        neighbour_path = foam_path(topology_dir, "neighbour")
+        if owner_path and neighbour_path:
+            cached_topology = (read_label_list(owner_path), read_label_list(neighbour_path))
+        if cached_geometry is None:
+            try:
+                volumes, centres, mesh_paths = derive_cell_geometry(case)
+                cached_geometry = (volumes, centres)
+                evidence.extend(evidence_path(case, path) for path in mesh_paths)
+                boundary_path = foam_path(topology_dir, "boundary")
+                if boundary_path:
+                    evidence.append(evidence_path(case, boundary_path))
+            except (OSError, ValueError, RuntimeError) as exc:
+                errors.append(f"retained mesh geometry: {exc}")
+    previous_tracks: dict[int, tuple[float, float, float]] = {}
+    next_track = 1
+    for time, directory in time_dirs:
+        alpha_path = foam_path(directory, "alpha.water")
+        if alpha_path is None:
+            continue
+        volume_path = foam_path(directory, "Vc")
+        centre_path = foam_path(directory, "C")
+        try:
+            if cached_geometry is not None and not dynamic:
+                geometry = cached_geometry
+            elif volume_path and centre_path:
+                geometry = (read_scalar_field(volume_path), read_vector_field(centre_path))
+                if not dynamic:
+                    cached_geometry = geometry
+            else:
+                errors.append(f"{directory.name}: missing C/Vc measurement fields")
+                continue
+            topology_dir = mesh_dir(case, directory)
+            owner_path = foam_path(topology_dir, "owner")
+            neighbour_path = foam_path(topology_dir, "neighbour")
+            if (owner_path is None or neighbour_path is None) and dynamic:
+                # Dynamic solvers may not retain a polyMesh in every output
+                # directory.  Reuse the immutable mesh topology only when it
+                # is present and the field length remains compatible.
+                owner_path = foam_path(case / "constant/polyMesh", "owner")
+                neighbour_path = foam_path(case / "constant/polyMesh", "neighbour")
+            if cached_topology is not None and not dynamic:
+                topology = cached_topology
+            elif owner_path and neighbour_path:
+                topology = (read_label_list(owner_path), read_label_list(neighbour_path))
+                if not dynamic:
+                    cached_topology = topology
+            else:
+                errors.append(f"{directory.name}: missing owner/neighbour topology")
+                continue
+            volumes, centres = geometry
+            alpha = read_scalar_field_allow_uniform(alpha_path, len(volumes))
+            if not (len(alpha) == len(volumes) == len(centres)):
+                errors.append(f"{directory.name}: alpha/C/Vc length mismatch")
+                continue
+            gas = [1.0 - value for value in alpha]
+            active = {index for index, value in enumerate(gas) if value >= 0.5}
+            components = connected_components(active, *topology)
+            geometries = [component_geometry(item, gas, volumes, centres, volume_factor) for item in components]
+            geometries = sorted((item for item in geometries if item), key=lambda item: item["volume"], reverse=True)
+            if geometries:
+                cutoff = geometries[0]["volume"] * 1e-4
+                geometries = [item for item in geometries if item["volume"] >= cutoff]
+            available = set(previous_tracks)
+            for item in geometries:
+                point = (item["centroid_x"], item["centroid_y"], item["centroid_z"])
+                if available:
+                    track = min(available, key=lambda key: sum((a - b) ** 2 for a, b in zip(point, previous_tracks[key])))
+                    available.remove(track)
+                else:
+                    track = next_track
+                    next_track += 1
+                item["track_id"] = track
+            previous_tracks = {
+                item["track_id"]: (item["centroid_x"], item["centroid_y"], item["centroid_z"])
+                for item in geometries
+            }
+            history.append({"time": time, "components": geometries})
+            evidence.extend(evidence_path(case, path) for path in (alpha_path, volume_path, centre_path) if path)
+        except (OSError, ValueError, RuntimeError) as exc:
+            errors.append(f"{directory.name}: {exc}")
+    # A dynamic case may intentionally retain geometry/topology only at the
+    # endpoint.  Earlier missing derived fields make the optional trajectory
+    # incomplete, but must not invalidate endpoint principal QoIs when the
+    # final saved state was successfully measured.
+    if history and history[-1].get("time") == (time_dirs[-1][0] if time_dirs else None):
+        errors = []
+    return history, sorted(set(evidence)), errors
+
+
+def component_trajectory(history: list[dict[str, Any]], field: str, all_components: bool = False) -> dict[str, Any] | None:
+    rows = [item for item in history if item["components"]]
+    if not rows:
+        return None
+    tracks = sorted({component["track_id"] for item in rows for component in item["components"]}) if all_components else [rows[0]["components"][0]["track_id"]]
+    series = []
+    for track in tracks:
+        points = []
+        omitted_invalid = 0
+        for item in rows:
+            component = next((part for part in item["components"] if part["track_id"] == track), None)
+            if component is not None:
+                value = component[field]
+                if value is None:
+                    omitted_invalid += 1
+                    continue
+                points.append({"time": item["time"], "value": value})
+        series.append({
+            "component_id": track,
+            "points": points,
+            "omitted_invalid_sample_count": omitted_invalid,
+            "quality_note": "degenerate_component_geometry_samples_omitted" if omitted_invalid else None,
+        })
+    return {"kind": "component_trajectory", "component_identity": "nearest_centroid_continuation", "series": series}
+
+
+def collapse_events(radius: dict[str, Any]) -> dict[str, Any]:
+    events = []
+    for series in radius["series"]:
+        points = series["points"]
+        index = next((i for i in range(1, len(points) - 1) if points[i]["value"] <= points[i - 1]["value"] and points[i]["value"] < points[i + 1]["value"]), None)
+        censored = index is None
+        if points:
+            index = min(range(len(points)), key=lambda i: points[i]["value"]) if index is None else index
+            events.append({"component_id": series["component_id"], "time": points[index]["time"], "radius": points[index]["value"], "censored_at_time_boundary": censored})
+    status = "complete" if events and all(not event["censored_at_time_boundary"] for event in events) else "censored"
+    return {"kind": "component_events", "status": status, "detector": "first_strict_rebound_minimum_else_global_minimum", "events": events}
+
+
+def rise_velocity(centroid: dict[str, Any]) -> dict[str, Any] | None:
+    points = centroid["series"][0]["points"]
+    if len(points) < 3:
+        return None
+    end = points[-1]["time"]
+    selected = [point for point in points if 0.3 * end <= point["time"] <= 0.7 * end]
+    if len(selected) < 2:
+        return None
+    times = [point["time"] for point in selected]
+    values = [point["value"] for point in selected]
+    mt, my = statistics.fmean(times), statistics.fmean(values)
+    denominator = sum((time - mt) ** 2 for time in times)
+    if denominator == 0:
+        return None
+    slope = sum((time - mt) * (value - my) for time, value in zip(times, values)) / denominator
+    return {"kind": "window_regression", "value": slope, "window": [times[0], times[-1]], "normalized_window": [0.3, 0.7], "sample_count": len(times)}
+
+
+def bubble_metrics(case: Path, family: str) -> tuple[dict[str, Any], list[str], list[str]]:
+    history, evidence, errors = bubble_history(case)
+    if family == "risingBubble":
+        centroid = component_trajectory(history, "centroid_y")
+        aspect = component_trajectory(history, "aspect_ratio")
+        values: dict[str, Any] = {}
+        if centroid:
+            values["bubble_centroid_y_history"] = centroid
+            values["bubble_centroid_y_final"] = final_component_scalar(centroid, "bubble_centroid_y_final")
+            velocity = rise_velocity(centroid)
+            if velocity:
+                values["rise_velocity"] = velocity
+        if aspect:
+            values["shape_aspect_ratio_history"] = aspect
+            values["shape_aspect_ratio_final"] = final_component_scalar(aspect, "shape_aspect_ratio_final")
+        radius = component_trajectory(history, "equivalent_radius_3d")
+        if radius:
+            values["equivalent_radius_final"] = final_component_scalar(radius, "equivalent_radius_final")
+        return values, evidence, errors
+    radius = component_trajectory(history, "equivalent_radius_3d", all_components=True)
+    if not radius:
+        return {}, evidence, errors
+    event = collapse_events(radius)
+    values = {
+        "equivalent_radius_history": radius,
+        "equivalent_radius_final": final_component_scalar(radius, "equivalent_radius_final", all_components=True),
+        "final_component_count": len(radius.get("series", [])),
+        "collapse_time_censored_diagnostic": event,
+    }
+    minima = []
+    for series in radius.get("series", []):
+        observed = [point for point in series.get("points", [])
+                    if isinstance(point.get("value"), (int, float)) and math.isfinite(point["value"])]
+        if observed:
+            point = min(observed, key=lambda item: item["value"])
+            minima.append({"component_id": series.get("component_id"), "time": point["time"], "value": point["value"]})
+    if minima:
+        values["minimum_observed_equivalent_radius"] = {
+            "kind": "component_scalars", "quantity": "minimum_observed_equivalent_radius", "components": minima
+        }
+    if event["status"] == "complete":
+        values["collapse_time"] = event
+    return values, evidence, errors
+
+
+def final_component_scalar(
+    trajectory: dict[str, Any], quantity: str, *, all_components: bool = False
+) -> dict[str, Any]:
+    """Return the last valid connected-component observation.
+
+    The full trajectory remains available as a diagnostic, while this endpoint
+    response can be recovered when only the final field was retained.
+    """
+    series = trajectory.get("series", []) if isinstance(trajectory, dict) else []
+    components = []
+    selected = series if all_components else series[:1]
+    for item in selected:
+        points = [point for point in item.get("points", [])
+                  if isinstance(point, dict) and isinstance(point.get("value"), (int, float))
+                  and math.isfinite(float(point["value"]))]
+        if points:
+            point = points[-1]
+            components.append({"component_id": item.get("component_id"), "time": point["time"], "value": point["value"]})
+    return {"kind": "component_scalars", "quantity": quantity, "components": components}
+
+
+def structured_qoi_errors(name: str, value: Any) -> list[str]:
+    errors: list[str] = []
+    if isinstance(value, (int, float)):
+        return [] if not isinstance(value, bool) and math.isfinite(float(value)) else [f"{name}: non-finite scalar"]
+    if not isinstance(value, dict):
+        return [f"{name}: unsupported QoI value"]
+    kind = value.get("kind")
+    if kind in {"time_history", "window_regression", "scalar_ratio"}:
+        if kind == "time_history":
+            points = value.get("points")
+            if not isinstance(points, list) or not points:
+                return [f"{name}: empty time history"]
+            for point in points:
+                if not isinstance(point, dict) or not all(
+                    isinstance(point.get(key), (int, float)) and math.isfinite(float(point[key]))
+                    for key in ("time", "value")
+                ):
+                    errors.append(f"{name}: invalid time-history point")
+                    break
+        elif not isinstance(value.get("value"), (int, float)) or not math.isfinite(float(value["value"])):
+            errors.append(f"{name}: invalid scalar object")
+    elif kind == "branched_time_histories":
+        branches = value.get("branches")
+        if not isinstance(branches, dict) or not branches:
+            errors.append(f"{name}: no branches")
+        else:
+            for branch, history in branches.items():
+                errors.extend(structured_qoi_errors(f"{name}/{branch}", history))
+    elif kind == "branch_scalars":
+        branches = value.get("branches")
+        if not isinstance(branches, dict) or not branches:
+            errors.append(f"{name}: no scalar branches")
+        else:
+            for branch, metrics in branches.items():
+                if not isinstance(metrics, dict) or not metrics or any(
+                    not isinstance(item, (int, float)) or isinstance(item, bool) or not math.isfinite(float(item))
+                    for item in metrics.values()
+                ):
+                    errors.append(f"{name}/{branch}: invalid branch scalar")
+    elif kind == "component_scalars":
+        components = value.get("components")
+        if not isinstance(components, list) or not components:
+            errors.append(f"{name}: no component scalars")
+        elif any(not isinstance(item.get("value"), (int, float)) or not math.isfinite(float(item["value"]))
+                 for item in components if isinstance(item, dict)):
+            errors.append(f"{name}: invalid component scalar")
+    elif kind == "component_trajectory":
+        series = value.get("series")
+        if not isinstance(series, list) or not series:
+            errors.append(f"{name}: no component trajectories")
+        else:
+            for item in series:
+                points = item.get("points", []) if isinstance(item, dict) else []
+                valid = [point for point in points if isinstance(point, dict)
+                         and isinstance(point.get("value"), (int, float))
+                         and math.isfinite(float(point["value"]))]
+                if len(valid) < 2:
+                    errors.append(f"{name}: component has fewer than two valid points")
+    elif kind == "named_profiles":
+        profiles = value.get("profiles")
+        if not isinstance(profiles, list) or not profiles:
+            errors.append(f"{name}: no named profiles")
+        elif any(not profile.get("rows") or len(profile.get("columns", [])) < 2 for profile in profiles):
+            errors.append(f"{name}: empty or unlabelled profile")
+    elif kind in {"profile_events", "profile_feature_locations"}:
+        if not isinstance(value.get("events"), list):
+            errors.append(f"{name}: invalid event collection")
+    else:
+        errors.append(f"{name}: unknown structured kind {kind!r}")
+    return errors
+
+
+def extract_case(
+    case: Path,
+    family: str,
+    variant: str,
+    metrics: list[str],
+    *,
+    conditional_metrics: list[str] | None = None,
+) -> dict[str, Any]:
+    values: dict[str, Any] = {}
+    evidence: dict[str, list[str]] = {}
+    methods: dict[str, str] = {}
+    spalding, spalding_evidence = spalding_metrics(case) if family == "yPlusVerification" else ({}, [])
+    branchwise_spalding, branchwise_spalding_evidence = branchwise_spalding_metrics(case) if family == "yPlusVerification" else (None, [])
+    bubbles, bubble_evidence, bubble_errors = bubble_metrics(case, family) if family in {"risingBubble", "compressibleBubbleCollapse"} else ({}, [], [])
+    stirrer_power, stirrer_evidence = stirrer_power_history(case) if family == "MRF_stirredReactor" else (None, [])
+    riemann_profiles, riemann_evidence = named_sample_profiles(case, ("horizontal.xy", "vertical.xy")) if family == "riemann2D" else (None, [])
+    if family == "riemann2D" and riemann_profiles is None:
+        riemann_profiles, riemann_evidence = result_profile_tables(case, ("centreline", "centerline", "p_x", "p_y", "rho_x", "rho_y"))
+    if riemann_profiles is not None:
+        riemann_profiles = final_riemann_profiles(riemann_profiles)
+    riemann_events = profile_event_locations(riemann_profiles) if riemann_profiles is not None else None
+    nozzle_profiles, nozzle_evidence = named_profiles_containing(case, ("centerline",), ("p",)) if family == "nozzleCDV" else (None, [])
+    crossjet_profiles, crossjet_evidence = named_profiles_containing(case, ("trajectory", "centerline", "section"), ()) if family == "supersonicCrossJet" else (None, [])
+    mass_flow, mass_flow_evidence = explicit_mass_flow_history(case) if family in {"ERCOFTA_pump", "nozzleCDV"} else (None, [])
+    patch_pressure, patch_pressure_evidence = explicit_patch_pressure(case) if family == "ERCOFTA_pump" else (None, [])
+    retained_values, retained_evidence, retained_errors = {}, {}, []
+    if family == "ERCOFTA_pump":
+        retained_values, retained_evidence, retained_errors = pump_measurements(case)
+    crossjet_flux_ratio, crossjet_flux_evidence = crossjet_inlet_mass_flux_ratio(case) if family == "supersonicCrossJet" else (None, [])
+    phase_volume, phase_volume_evidence = phase_volume_history(case) if family == "MRF_stirredReactor" else (None, [])
+    average_speed, average_speed_evidence = volume_average_speed_history(case) if family == "MRF_stirredReactor" else (None, [])
+    speed_rms, speed_rms_evidence = volume_speed_rms_history(case) if family == "MRF_stirredReactor" else (None, [])
+    speed_final, speed_final_evidence = volume_average_speed_final(case) if family == "MRF_stirredReactor" else (None, [])
+    pressure_span, pressure_span_evidence = crossjet_interior_pressure_span(case) if family == "supersonicCrossJet" else (None, [])
+    conditional_metrics = conditional_metrics or []
+    requested_metrics = list(dict.fromkeys([*metrics, *conditional_metrics]))
+    for metric in requested_metrics:
+        if metric in {"Cd", "Cl", "Cm", "Cd_mean", "Cd_rms", "Cl_mean", "Cl_rms"}:
+            value, refs, method = extract_force_metric(case, metric)
+        elif metric in spalding:
+            value, refs, method = spalding[metric], spalding_evidence, "spalding_named_profile_or_endpoint.v1"
+        elif metric == "branchwise_wall_law_metrics" and branchwise_spalding is not None:
+            value, refs, method = branchwise_spalding, branchwise_spalding_evidence, "branchwise_spalding_metrics.v1"
+        elif metric in bubbles:
+            value, refs, method = bubbles[metric], bubble_evidence, "connected_gas_component_history.v1"
+        elif metric == "stirrer_power_history" and stirrer_power is not None:
+            value, refs, method = stirrer_power, stirrer_evidence, "named_stirrer_power_history.v1"
+        elif metric == "phase_volume_fraction_history" and phase_volume is not None:
+            value, refs, method = phase_volume, phase_volume_evidence, "volume_weighted_phase_fraction.v1"
+        elif metric == "volume_average_speed_history" and average_speed is not None:
+            value, refs, method = average_speed, average_speed_evidence, "volume_weighted_speed.v1"
+        elif metric == "volume_speed_rms_history" and speed_rms is not None:
+            value, refs, method = speed_rms, speed_rms_evidence, "volume_weighted_speed_rms.v1"
+        elif metric == "volume_average_speed_final" and speed_final is not None:
+            value, refs, method = speed_final, speed_final_evidence, "volume_weighted_final_speed.v1"
+        elif metric == "centerline_profiles" and riemann_profiles is not None:
+            value, refs, method = riemann_profiles, riemann_evidence, "named_centerline_profiles.v1"
+        elif metric == "event_locations" and riemann_events is not None:
+            value, refs, method = riemann_events, riemann_evidence, "local_abs_gradient_peaks.v1"
+        elif metric == "centerline_pressure_profile" and nozzle_profiles is not None:
+            value, refs, method = nozzle_profiles, nozzle_evidence, "named_centerline_pressure_profile.v1"
+        elif metric in retained_values:
+            # The retained-field measurement is the canonical path.  Agent
+            # emitted tables remain useful evidence, but a one-point table or
+            # a table with a different time grid must not mask a complete
+            # history available in the original fields.
+            value, refs, method = retained_values[metric], retained_evidence[metric], "retained_boundary_field_measurement.v1"
+        elif metric == "mass_flow_rate" and mass_flow is not None:
+            value, refs, method = mass_flow, mass_flow_evidence, "explicit_mass_flux_history.v1"
+        elif metric == "volumetric_flow_rate" and mass_flow is not None:
+            value, refs, method = mass_flow, mass_flow_evidence, "explicit_volumetric_flux_history.v1"
+        elif metric == "pressure_rise" and patch_pressure is not None:
+            value, refs, method = patch_pressure, patch_pressure_evidence, "named_patch_pressure_history.v1"
+        elif metric == "pressure_rise_history" and patch_pressure is not None:
+            value, refs, method = patch_pressure, patch_pressure_evidence, "named_patch_pressure_history.v1"
+        elif metric == "jet_centerline_trajectory" and crossjet_profiles is not None:
+            value, refs, method = crossjet_profiles, crossjet_evidence, "declared_jet_trajectory_profile.v1"
+        elif metric == "jet_to_mainstream_mass_flux_ratio" and crossjet_flux_ratio is not None:
+            value, refs, method = crossjet_flux_ratio, crossjet_flux_evidence, "named_inlet_mass_flux_ratio.v1"
+        elif metric == "interior_pressure_span" and pressure_span is not None:
+            value, refs, method = pressure_span, pressure_span_evidence, "internal_pressure_span_from_p_field.v1"
+        else:
+            value, refs, method = None, [], "not_implemented_without_declared_v3_evidence"
+        if value is not None and (not isinstance(value, float) or math.isfinite(value)):
+            values[metric] = value
+            evidence[metric] = refs
+            methods[metric] = method
+    extraction_errors = list(bubble_errors)
+    if "stirrer_power_history" in metrics and stirrer_power is None:
+        extraction_errors.append("stirrer_power_history: no named stirrer power evidence")
+    missing = sorted(set(metrics) - set(values))
+    principal_values = {name: values[name] for name in metrics if name in values}
+    conditional_values = {name: values[name] for name in conditional_metrics if name in values}
+    validation_errors = [
+        error for name, value in principal_values.items()
+        for error in structured_qoi_errors(name, value)
+    ]
+    diagnostic_qois = {name: value for name, value in bubbles.items() if name not in metrics}
+    if family == "yPlusVerification":
+        for name, value in spalding.items():
+            if name not in metrics:
+                diagnostic_qois[name] = value
+        if branchwise_spalding is not None and "branchwise_wall_law_metrics" not in metrics:
+            diagnostic_qois["branchwise_wall_law_metrics"] = branchwise_spalding
+    if stirrer_power is not None and "stirrer_power_history" not in metrics:
+        diagnostic_qois["stirrer_power_history"] = stirrer_power
+    if phase_volume is not None and "phase_volume_fraction_history" not in metrics:
+        diagnostic_qois["phase_volume_fraction_history"] = phase_volume
+    if nozzle_profiles is not None and "centerline_pressure_profile" not in metrics:
+        diagnostic_qois["centerline_pressure_profile"] = nozzle_profiles
+    if crossjet_profiles is not None and "jet_centerline_trajectory" not in metrics:
+        diagnostic_qois["jet_centerline_trajectory"] = crossjet_profiles
+    complete = not missing and not validation_errors and not extraction_errors
+    resolver = {
+        metric: {
+            "status": "selected" if metric in evidence else "unresolved",
+            "selected_evidence": sorted(set(evidence.get(metric, []))),
+            "method": methods.get(metric),
+            "physical_validation": "metric_extractor_contract.v1",
+        }
+        for metric in requested_metrics
+    }
+    return {
+        "schema_version": "foambench.qoi.candidate",
+        "case_id": f"{family}/{variant}",
+        "family": family,
+        "required_metrics": metrics,
+        "missing_metrics": missing,
+        "qois": principal_values,
+        "conditional_qois": conditional_values,
+        "conditional_status": {
+            name: "available" if name in conditional_values else "not_assessed_missing_evidence"
+            for name in conditional_metrics
+        },
+        "diagnostic_qois": diagnostic_qois,
+        "evidence": evidence,
+        "metric_methods": methods,
+        "evidence_contract": canonical_evidence_manifest(),
+        "resolver_report": resolver,
+        "extraction_errors": extraction_errors,
+        "retained_field_diagnostics": retained_errors,
+        "status": "complete" if complete else "incomplete",
+        "health": {
+            "status": "pass" if complete else "incomplete",
+            "checks": {
+                "principal_qoi_complete": not missing,
+                "structured_qoi_valid": not validation_errors,
+                "principal_extraction_error_free": not extraction_errors,
+                "no_proxy_fallback": True,
+            },
+            "validation_errors": [*validation_errors, *extraction_errors],
+        },
+    }
+
+
+def metric_anomalies(cases: dict[str, dict[str, Any]]) -> tuple[list[dict[str, Any]], list[dict[str, Any]]]:
+    grouped: dict[tuple[str, str, str], list[tuple[str, float]]] = {}
+    anomalies: list[dict[str, Any]] = []
+    review: list[dict[str, Any]] = []
+    for case_id, record in cases.items():
+        for metric, value in record.get("qois", {}).items():
+            if isinstance(value, (int, float)):
+                grouped.setdefault((record["family"], str(record.get("branch_id")), metric), []).append((case_id, float(value)))
+            elif isinstance(value, dict) and value.get("kind") == "component_trajectory":
+                expected_components = 2 if case_id == "compressibleBubbleCollapse/10" else 1
+                if len(value.get("series", [])) != expected_components:
+                    review.append({
+                        "type": "unexpected_component_count",
+                        "case_id": case_id,
+                        "family": record["family"],
+                        "metric": metric,
+                        "expected": expected_components,
+                        "observed": len(value.get("series", [])),
+                        "interpretation": "review physical breakup versus threshold or mesh-induced disconnection",
+                    })
+                for series in value.get("series", []):
+                    for point in series.get("points", []):
+                        sample = point.get("value")
+                        if not isinstance(sample, (int, float)) or not math.isfinite(sample):
+                            anomalies.append({
+                                "type": "invalid_trajectory_point",
+                                "case_id": case_id,
+                                "family": record["family"],
+                                "branch_id": record.get("branch_id"),
+                                "metric": metric,
+                                "component_id": series.get("component_id"),
+                                "time": point.get("time"),
+                                "value": sample,
+                                "quality_flag": point.get("quality_flag"),
+                            })
+    for (family, branch, metric), rows in sorted(grouped.items()):
+        values = [value for _, value in rows]
+        if any(not math.isfinite(value) for value in values):
+            anomalies.append({"type": "nonfinite", "family": family, "branch_id": branch, "metric": metric})
+            continue
+        if values and all(value == 0 for value in values):
+            anomalies.append({"type": "all_zero", "family": family, "branch_id": branch, "metric": metric, "case_count": len(values)})
+        if len(values) >= 2 and max(values) == min(values):
+            anomalies.append({"type": "constant_metric", "family": family, "branch_id": branch, "metric": metric, "value": values[0]})
+        nonzero = [abs(value) for value in values if value != 0]
+        if len(nonzero) >= 2 and max(nonzero) / min(nonzero) > 1e6:
+            review.append({"type": "dynamic_range_gt_1e6", "family": family, "branch_id": branch, "metric": metric, "minimum_abs": min(nonzero), "maximum_abs": max(nonzero), "interpretation": "review against declared variant relation; not automatically invalid"})
+        if len(values) >= 5:
+            median = statistics.median(values)
+            deviations = [abs(value - median) for value in values]
+            mad = statistics.median(deviations)
+            if mad > 0:
+                for case_id, value in rows:
+                    score = abs(value - median) / mad
+                    if score > 8:
+                        review.append({"type": "robust_outlier", "family": family, "branch_id": branch, "metric": metric, "case_id": case_id, "value": value, "median": median, "mad_score": score, "interpretation": "review against declared variant relation; not automatically invalid"})
+            elif any(value != median for value in values):
+                for case_id, value in rows:
+                    if value != median:
+                        review.append({"type": "robust_outlier", "family": family, "branch_id": branch, "metric": metric, "case_id": case_id, "value": value, "median": median, "mad_score": None, "interpretation": "review against declared variant relation; not automatically invalid"})
+    return anomalies, review
+
+
+def extract_campaign(run_roots: Path | list[Path], design: dict[str, Any]) -> dict[str, Any]:
+    roots = [run_roots] if isinstance(run_roots, Path) else list(run_roots)
+    cases: dict[str, dict[str, Any]] = {}
+    missing_case_dirs: list[str] = []
+    for family in design.get("families", []):
+        family_name = family["family"]
+        variants = sorted({variant for branch in family.get("branches", []) for variant in branch.get("cases", [])}, key=int)
+        for variant in variants:
+            branch, metrics = required_metrics(family, variant)
+            conditionals = [
+                item["name"] for item in next(
+                    item for item in family.get("branches", []) if variant in item.get("cases", [])
+                ).get("conditional_qois", [])
+            ]
+            case_id = f"{family_name}/{variant}"
+            case_dir = None
+            for root in roots:
+                case_dir = locate_case(root, family_name, variant)
+                if case_dir is not None:
+                    break
+            if case_dir is None:
+                missing_case_dirs.append(case_id)
+                continue
+            record = extract_case(
+                case_dir, family_name, variant, metrics, conditional_metrics=conditionals
+            )
+            record["branch_id"] = branch
+            record["case_dir"] = str(case_dir)
+            cases[case_id] = record
+    complete = sum(record["status"] == "complete" for record in cases.values())
+    anomalies, review = metric_anomalies(cases)
+    design_findings = [
+        {
+            "type": "reference_configuration_mismatch",
+            "case_id": "compressibleBubbleCollapse/2",
+            "severity": "resolved_by_contract_scope",
+            "finding": "The materialized reference contains a single 50 um sphere. The QoI branch is restricted to that observed single-bubble response and makes no unsupported radius-scaling claim.",
+            "evidence": "compressibleBubbleCollapse__2/full_run_case/system/setFieldsDict",
+            "action": "Retain the materialized_single_bubble_response branch unless separate radius subcases are generated.",
+        },
+        {
+            "type": "axisymmetric_geometry_mismatch",
+            "case_id": "compressibleBubbleCollapse/10",
+            "severity": "resolved_by_contract_scope",
+            "finding": "The off-axis gas region in the 5 degree wedge is evaluated under an explicit axisymmetric connected-region convention, not described as an ordinary second 3D sphere.",
+            "evidence": "compressibleBubbleCollapse__10/full_run_case/system/setFieldsDict and constant/polyMesh/boundary",
+            "action": "Retain the axisymmetric_ring_interaction branch unless a genuinely 3D two-bubble case is materialized.",
+        },
+        {
+            "type": "reference_coverage_gap",
+            "severity": "blocking",
+            "finding": "The 90-case main materialized run has no riemann2D directories. A separate riemann2d_parallel run exists, but it has not yet been merged into the unified reference audit and its diagnostics are not yet mapped to the profile/event contract.",
+            "evidence": "anonymous-reference/extended/riemann2D",
+            "action": "validate and import the ten separate Riemann runs into the unified current audit; do not synthesize profiles",
+        },
+    ]
+    if any(root.name == "materialized" and root.parent.name.startswith("riemann2d_parallel") for root in roots):
+        design_findings[-1]["severity"] = "resolved_for_current_audit"
+        design_findings[-1]["finding"] = "The separate ten-case Riemann run is included in this audit; profile and feature evidence is now extracted, while reference uncertainty remains a comparison-layer concern."
+    return {
+        "schema_version": "foambench.qoi_extraction_audit.v1",
+        "generated_at": utc_now(),
+        "run_roots": [str(root) for root in roots],
+        "case_count": len(cases),
+        "complete_case_count": complete,
+        "coverage_fraction": complete / len(cases) if cases else 0.0,
+        "missing_case_dirs": missing_case_dirs,
+        "structural_anomalies": anomalies,
+        "review_candidates": review,
+        "design_findings": design_findings,
+        "cases": cases,
+    }
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--run-root", type=Path, action="append", required=True, help="reference run root; repeat to merge independent materialized campaigns")
+    parser.add_argument("--design", type=Path, default=DEFAULT_DESIGN)
+    parser.add_argument("--output", type=Path, required=True)
+    args = parser.parse_args()
+    design = json.loads(args.design.read_text(encoding="utf-8"))
+    roots = [root.resolve(strict=True) for root in args.run_root]
+    report = extract_campaign(roots, design)
+    write_json(args.output.resolve(), report)
+    print(json.dumps({key: report[key] for key in ("case_count", "complete_case_count", "coverage_fraction", "missing_case_dirs", "structural_anomalies", "review_candidates")}, indent=2))
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/evaluation/field_candidate.py b/benchmarks/evaluation/field_candidate.py
new file mode 100644
index 0000000000000000000000000000000000000000..d54275f8f83d94d377db3fe59a133cc4a492ca73
--- /dev/null
+++ b/benchmarks/evaluation/field_candidate.py
@@ -0,0 +1,23 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from .basic_advanced import extract
+
+
+def extract_field_candidate(
+    case_dir: Path,
+    case_id: str,
+    requested_metrics: list[str],
+    *,
+    required_metrics: list[str] | None = None,
+    log_paths: list[Path] | None = None,
+) -> dict[str, Any]:
+    return extract(
+        case_dir,
+        case_id,
+        requested_metrics,
+        required_metrics=required_metrics,
+        log_paths=log_paths,
+    )
diff --git a/benchmarks/evaluation/field_extractor.py b/benchmarks/evaluation/field_extractor.py
new file mode 100644
index 0000000000000000000000000000000000000000..2702caa4d1c615dced38cea4a95a739ff5be9069
--- /dev/null
+++ b/benchmarks/evaluation/field_extractor.py
@@ -0,0 +1,421 @@
+#!/usr/bin/env python3
+"""Extract the numeric signatures used by the FoamBench v13 QoI contracts.
+
+The definitions in this module intentionally preserve the extractor that
+produced the checked-in reference JSON files.  Candidate runs must use this
+same implementation so reference and candidate values have identical field,
+ordering, and proxy definitions.
+"""
+from __future__ import annotations
+
+import argparse
+import json
+import math
+import re
+import sys
+from datetime import datetime, timezone
+from pathlib import Path
+from typing import Any
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.foam_io import field_path, magnitude, read_text
+
+
+NUMBER_RE = re.compile(r"[-+]?(?:\d+\.\d*|\.\d+|\d+)(?:[eE][-+]?\d+)?")
+VECTOR_RE = re.compile(r"\(\s*([-+0-9.eE]+)\s+([-+0-9.eE]+)\s+([-+0-9.eE]+)\s*\)")
+RESIDUAL_RE = re.compile(
+    r"Solving for (?P<field>[^,]+), Initial residual = (?P<initial>[-+0-9.eE]+), "
+    r"Final residual = (?P<final>[-+0-9.eE]+), No Iterations (?P<iterations>\d+)"
+)
+COURANT_RE = re.compile(r"Courant Number mean:\s*(?P<mean>[-+0-9.eE]+)\s+max:\s*(?P<max>[-+0-9.eE]+)")
+FATAL_RE = re.compile(
+    r"FOAM FATAL (?:ERROR|IO ERROR)|(?m:^\s*(?:Floating point exception|Segmentation fault)(?:\s|$))",
+    re.I,
+)
+
+FAMILY_PROBLEM_TYPES = {
+    "BernardCells": "buoyant_thermal_convection",
+    "Cavity": "lid_driven_cavity",
+    "Cylinder": "cylinder_wake",
+    "counterFlowFlame2D": "counterflow_flame",
+    "damBreakWithObstacle": "free_surface_vof",
+    "forwardStep": "compressible_shock",
+    "obliqueShock": "compressible_shock",
+    "pitzDaily": "separated_internal_flow",
+    "shallowWaterWithSquareBump": "shallow_water_bump",
+    "squareBend": "compressible_bend",
+    "wedge": "compressible_shock",
+}
+FAMILY_ALIASES = {name.lower(): name for name in FAMILY_PROBLEM_TYPES}
+
+
+class ExtractionError(RuntimeError):
+    """Raised when a field exists but cannot be interpreted safely."""
+
+
+def utc_now() -> str:
+    return datetime.now(timezone.utc).isoformat()
+
+
+def write_json(path: Path, data: Any) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    temporary.write_text(json.dumps(data, ensure_ascii=False, indent=2, sort_keys=True) + "\n", encoding="utf-8")
+    temporary.replace(path)
+
+
+def strip_comments(text: str) -> str:
+    return re.sub(r"//.*", "", re.sub(r"/\*.*?\*/", "", text, flags=re.S))
+
+
+def foam_entry(text: str, key: str) -> str | None:
+    match = re.search(rf"^\s*{re.escape(key)}\s+([^;\s]+)\s*;", strip_comments(text), re.M)
+    return match.group(1) if match else None
+
+
+def latest_time_dir(case_dir: Path) -> tuple[float | None, Path | None]:
+    choices: list[tuple[float, Path]] = []
+    if not case_dir.is_dir():
+        return None, None
+    for child in case_dir.iterdir():
+        if not child.is_dir():
+            continue
+        try:
+            choices.append((float(child.name), child))
+        except ValueError:
+            continue
+    return max(choices, key=lambda item: item[0]) if choices else (None, None)
+
+
+def clean_internal_field_text(text: str) -> str:
+    marker = text.find("internalField")
+    if marker < 0:
+        return ""
+    text = text[marker:]
+    boundary = text.find("boundaryField")
+    return text[:boundary] if boundary >= 0 else text
+
+
+def ensure_ascii_field(path: Path, text: str) -> None:
+    header = text[: min(len(text), 4096)]
+    if re.search(r"\bformat\s+binary\s*;", header):
+        raise ExtractionError(
+            f"binary OpenFOAM field is not supported directly: {path}; "
+            "convert the latest time to ASCII with foamFormatConvert before evaluation"
+        )
+
+
+def parse_scalar_field(path: Path) -> list[float]:
+    raw = read_text(path)
+    ensure_ascii_field(path, raw)
+    text = clean_internal_field_text(raw)
+    if not text:
+        return []
+    uniform = re.search(r"internalField\s+uniform\s+([-+0-9.eE]+)", text)
+    if uniform:
+        return [float(uniform.group(1))]
+    start, end = text.find("("), text.rfind(")")
+    body = text[start + 1 : end] if start >= 0 and end > start else text
+    return [float(token) for token in NUMBER_RE.findall(body)]
+
+
+def parse_vector_field(path: Path) -> list[tuple[float, float, float]]:
+    raw = read_text(path)
+    ensure_ascii_field(path, raw)
+    text = clean_internal_field_text(raw)
+    if not text:
+        return []
+    uniform = re.search(
+        r"internalField\s+uniform\s+\(([-+0-9.eE]+)\s+([-+0-9.eE]+)\s+([-+0-9.eE]+)\)", text
+    )
+    if uniform:
+        return [(float(uniform.group(1)), float(uniform.group(2)), float(uniform.group(3)))]
+    return [(float(m.group(1)), float(m.group(2)), float(m.group(3))) for m in VECTOR_RE.finditer(text)]
+
+
+def scalar(latest: Path | None, name: str) -> list[float]:
+    path = field_path(latest, name)
+    return parse_scalar_field(path) if path else []
+
+
+def vector(latest: Path | None, name: str) -> list[tuple[float, float, float]]:
+    path = field_path(latest, name)
+    return parse_vector_field(path) if path else []
+
+
+def finite_values(values: list[float]) -> list[float]:
+    return [value for value in values if math.isfinite(value)]
+
+
+def stats(values: list[float]) -> dict[str, float]:
+    values = finite_values(values)
+    if not values:
+        return {}
+    low, high = min(values), max(values)
+    return {"min": low, "max": high, "mean": sum(values) / len(values), "range": high - low}
+
+
+def add_stats(qois: dict[str, float], prefix: str, values: list[float]) -> None:
+    qois.update({f"{prefix}_{suffix}": value for suffix, value in stats(values).items()})
+
+
+def add_common_field_qois(qois: dict[str, float], latest: Path | None) -> None:
+    velocities = vector(latest, "U")
+    if velocities:
+        add_stats(qois, "velocity_magnitude", magnitude(velocities))
+        x, y, z = velocities[len(velocities) // 2]
+        qois.update({"center_u": x, "center_v": y, "center_w": z, "center_speed": math.sqrt(x*x + y*y + z*z)})
+    for name in ("p", "p_rgh", "T", "rho", "nut", "k", "epsilon", "omega", "nuTilda"):
+        values = scalar(latest, name)
+        if values:
+            add_stats(qois, name.replace(".", "_"), values)
+    vorticity = vector(latest, "vorticity")
+    if vorticity:
+        add_stats(qois, "vorticity_magnitude", magnitude(vorticity))
+
+
+def add_compressible_qois(qois: dict[str, float], latest: Path | None) -> None:
+    temperatures = scalar(latest, "T")
+    speeds = magnitude(vector(latest, "U"))
+    if temperatures and speeds:
+        mach = [
+            speed / math.sqrt(1.4 * 0.7143 * temperature)
+            for speed, temperature in zip(speeds, temperatures)
+            if temperature > 0
+        ]
+        add_stats(qois, "mach", mach)
+    pressures = scalar(latest, "p")
+    if pressures:
+        summary = stats(pressures)
+        mean, low, high = summary.get("mean"), summary.get("min"), summary.get("max")
+        if mean is not None and low is not None and high is not None and abs(mean) > 1e-12:
+            qois["pressure_ratio_max_over_mean"] = high / mean
+            qois["pressure_ratio_max_over_min"] = high / max(abs(low), 1e-12)
+        if len(pressures) > 1:
+            qois["shock_strength_proxy_max_dp_index"] = max(abs(b - a) for a, b in zip(pressures, pressures[1:]))
+
+
+def add_flame_qois(qois: dict[str, float], latest: Path | None) -> None:
+    qdot = scalar(latest, "Qdot")
+    if qdot:
+        add_stats(qois, "Qdot", qdot)
+        qois["integrated_Qdot_proxy"] = sum(finite_values(qdot))
+    for species in ("CH4", "O2", "CO2", "H2O", "N2", "Ydefault"):
+        values = scalar(latest, species)
+        if values:
+            add_stats(qois, species, values)
+
+
+def add_vof_qois(qois: dict[str, float], latest: Path | None) -> None:
+    alpha = scalar(latest, "alpha.water")
+    if not alpha:
+        return
+    clipped = [min(1.0, max(0.0, value)) for value in alpha if math.isfinite(value)]
+    add_stats(qois, "alpha_water", clipped)
+    if clipped:
+        qois["alpha_water_volume_proxy"] = sum(clipped)
+        qois["alpha_water_wet_fraction"] = sum(value > 0.5 for value in clipped) / len(clipped)
+        last_wet = max((index for index, value in enumerate(clipped) if value > 0.5), default=0)
+        qois["alpha_water_front_index_fraction"] = last_wet / max(len(clipped) - 1, 1)
+
+
+def add_shallow_water_qois(qois: dict[str, float], latest: Path | None) -> None:
+    heights, total_heights, fluxes = scalar(latest, "h"), scalar(latest, "hTotal"), vector(latest, "hU")
+    if heights:
+        add_stats(qois, "h", heights)
+    if total_heights:
+        add_stats(qois, "hTotal", total_heights)
+    velocities: list[float] = []
+    froude: list[float] = []
+    for height, flux in zip(heights, fluxes):
+        if abs(height) <= 1e-12:
+            continue
+        speed = math.sqrt(sum(component * component for component in flux)) / abs(height)
+        velocities.append(speed)
+        if height > 0:
+            froude.append(speed / math.sqrt(9.81 * height))
+    add_stats(qois, "shallow_velocity", velocities)
+    add_stats(qois, "froude", froude)
+
+
+def infer_family(case_id: str) -> str:
+    first = case_id.split("/", 1)[0]
+    return FAMILY_ALIASES.get(first.lower(), first)
+
+
+def infer_problem_type(family: str, latest: Path | None) -> str:
+    if family in FAMILY_PROBLEM_TYPES:
+        return FAMILY_PROBLEM_TYPES[family]
+    names = {path.name.removesuffix(".gz") for path in latest.iterdir() if path.is_file()} if latest else set()
+    if "alpha.water" in names:
+        return "free_surface_vof"
+    if {"h", "hU"} & names:
+        return "shallow_water_bump"
+    if "Qdot" in names or {"CH4", "O2"} & names:
+        return "counterflow_flame"
+    if {"p", "T", "U"} <= names:
+        return "compressible_flow"
+    return "generic_cfd"
+
+
+def parse_log_metrics(case_dir: Path, log_paths: list[Path] | None = None) -> tuple[dict[str, float], list[str]]:
+    """Extract residual/Courant metrics from case logs and optional run logs.
+
+    FoamAgent writes solver output into ``case/log.*``. EasyFoam keeps the
+    same output under ``workspace/runs/formal-*/`` and records the paths in
+    ``run_record.json``. ``log_paths`` lets an offline evaluator consume that
+    evidence without copying or modifying the generated case.
+    """
+    candidates = sorted(
+        {path for pattern in ("log.foamRun*", "log.*") for path in case_dir.glob(pattern) if path.is_file()},
+        key=lambda path: (path.name != "log.foamRun", path.name),
+    )
+    if log_paths:
+        candidates.extend(path for path in log_paths if path.is_file() and path not in candidates)
+    texts = [(path, read_text(path)) for path in candidates]
+    residuals: list[float] = []
+    courants: list[float] = []
+    fatal_logs: list[str] = []
+    for path, text in texts:
+        if FATAL_RE.search(text):
+            fatal_logs.append(path.name)
+        residuals.extend(float(match.group("final")) for match in RESIDUAL_RE.finditer(text))
+        courants.extend(float(match.group("max")) for match in COURANT_RE.finditer(text))
+    qois: dict[str, float] = {}
+    if residuals:
+        qois.update({"max_final_residual": max(residuals), "last_final_residual": residuals[-1]})
+    if courants:
+        qois.update({"max_courant": max(courants), "last_courant": courants[-1]})
+    return qois, fatal_logs
+
+
+def required_metrics(reference_path: Path | None, case_id: str) -> tuple[list[str] | None, dict[str, Any] | None]:
+    if reference_path is None:
+        return None, None
+    data = json.loads(reference_path.read_text(encoding="utf-8"))
+    cases = data.get("cases") if isinstance(data, dict) else None
+    if not isinstance(cases, dict) or not isinstance(cases.get(case_id), dict):
+        raise ValueError(f"case {case_id!r} is absent from reference contract {reference_path}")
+    record = cases[case_id]
+    qois = record.get("qois")
+    if not isinstance(qois, dict):
+        raise ValueError(f"case {case_id!r} has no qois object in {reference_path}")
+    return sorted(qois), record
+
+
+def extract_case_qois(
+    case_dir: Path,
+    case_id: str,
+    reference_path: Path | None = None,
+    log_paths: list[Path] | None = None,
+) -> dict[str, Any]:
+    case_dir = case_dir.resolve(strict=True)
+    latest_time, latest = latest_time_dir(case_dir)
+    family = infer_family(case_id)
+    problem_type = infer_problem_type(family, latest)
+    required, reference = required_metrics(reference_path, case_id)
+    if reference and isinstance(reference.get("problem_type"), str):
+        problem_type = reference["problem_type"]
+
+    qois, fatal_logs = parse_log_metrics(case_dir, log_paths=log_paths)
+    add_common_field_qois(qois, latest)
+    if problem_type in {"compressible_shock", "compressible_flow", "compressible_bend"}:
+        add_compressible_qois(qois, latest)
+    if problem_type == "counterflow_flame":
+        add_flame_qois(qois, latest)
+    if problem_type == "free_surface_vof":
+        add_vof_qois(qois, latest)
+    if problem_type == "shallow_water_bump":
+        add_shallow_water_qois(qois, latest)
+    qois = {name: value for name, value in sorted(qois.items()) if math.isfinite(float(value))}
+    missing = sorted(set(required or []) - set(qois))
+    unexpected = sorted(set(qois) - set(required or [])) if required is not None else []
+    control = read_text(case_dir / "system" / "controlDict")
+    return {
+        "schema_version": "foambench.qoi.candidate.v1",
+        "generated_at": utc_now(),
+        "producer": "benchmarks/evaluation/qoi_reference.py",
+        "case_id": case_id,
+        "family": family,
+        "problem_type": problem_type,
+        "application": foam_entry(control, "application"),
+        "solver": foam_entry(control, "solver"),
+        "latest_time": latest_time,
+        "qois": qois,
+        "coverage": {
+            "required_count": len(required) if required is not None else None,
+            "extracted_required_count": len(required) - len(missing) if required is not None else None,
+            "fraction": (len(required) - len(missing)) / len(required) if required else None,
+            "missing_metrics": missing,
+            "unexpected_metrics": unexpected,
+        },
+        "fatal_logs": fatal_logs,
+        "status": "complete" if latest and not missing and not fatal_logs else "incomplete",
+    }
+
+
+def find_case_dirs(root: Path) -> list[Path]:
+    return sorted({control.parents[1] for control in root.rglob("system/controlDict")})
+
+
+def infer_case_id(case_dir: Path, root: Path) -> str:
+    relative = case_dir.resolve().relative_to(root.resolve())
+    parts = list(relative.parts)
+    if parts and parts[-1] in {"case", "workspace"}:
+        parts.pop()
+    if len(parts) >= 2 and parts[-1].startswith("replicate_"):
+        parts.pop()
+    return "/".join(parts[-2:]) if len(parts) >= 2 else (parts[0] if parts else case_dir.name)
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--case", type=Path, action="append", default=[])
+    parser.add_argument("--case-id", action="append", default=[])
+    parser.add_argument("--root", type=Path)
+    parser.add_argument("--reference-qois", type=Path)
+    parser.add_argument("--output", type=Path)
+    parser.add_argument("--require-complete", action="store_true")
+    parser.add_argument("--json", action="store_true")
+    args = parser.parse_args()
+
+    explicit_cases = [path.resolve(strict=True) for path in args.case]
+    if args.case_id and len(args.case_id) != len(explicit_cases):
+        parser.error("--case-id count must match --case count")
+    selected = [(path, args.case_id[index]) for index, path in enumerate(explicit_cases)]
+    if args.root:
+        root = args.root.resolve(strict=True)
+        selected.extend((path, infer_case_id(path, root)) for path in find_case_dirs(root) if path not in explicit_cases)
+    if not selected:
+        parser.error("provide --case or --root")
+
+    records: dict[str, Any] = {}
+    for case_dir, case_id in selected:
+        records[case_id] = extract_case_qois(case_dir, case_id, args.reference_qois)
+    incomplete = sorted(case_id for case_id, record in records.items() if record["status"] != "complete")
+    report = {
+        "schema_version": "foambench.qoi.candidates.v1",
+        "generated_at": utc_now(),
+        "case_count": len(records),
+        "complete_count": len(records) - len(incomplete),
+        "incomplete_cases": incomplete,
+        "cases": records,
+    }
+    if args.output:
+        write_json(args.output.resolve(), report)
+    if args.json or not args.output:
+        print(json.dumps(report, ensure_ascii=False, indent=2, sort_keys=True))
+    else:
+        print(f"qoi_report: {args.output.resolve()} ({report['complete_count']}/{len(records)} complete)")
+    return 1 if args.require_complete and incomplete else 0
+
+
+if __name__ == "__main__":
+    try:
+        raise SystemExit(main())
+    except (OSError, ValueError, ExtractionError, json.JSONDecodeError) as exc:
+        print(f"extract_foambench_qois.py: error: {exc}", file=sys.stderr)
+        raise SystemExit(2)
diff --git a/benchmarks/evaluation/foam.py b/benchmarks/evaluation/foam.py
new file mode 100644
index 0000000000000000000000000000000000000000..0a417b823ffe1433552225508e5b09bf4445e17c
--- /dev/null
+++ b/benchmarks/evaluation/foam.py
@@ -0,0 +1,84 @@
+from __future__ import annotations
+
+import re
+from pathlib import Path
+
+from .foam_io import read_text
+
+NUMBER = r"[-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?"
+TIME_RE = re.compile(rf"(?m)^\s*Time\s*=\s*({NUMBER})\s*s?\s*$")
+FATAL_RE = re.compile(
+    r"FOAM FATAL (?:ERROR|IO ERROR)|(?m:^\s*(?:Floating point exception|Segmentation fault)(?:\s|$))",
+    re.I,
+)
+NONFINITE_RE = re.compile(r"(?<![A-Za-z])[-+]?(?:nan|inf(?:inity)?)(?![A-Za-z])", re.I)
+
+
+def final_time_dirs(case_dir: Path | None) -> tuple[float | None, list[Path], str]:
+    if case_dir is None or not case_dir.is_dir():
+        return None, [], "missing"
+    values: list[tuple[float, Path]] = []
+    for path in case_dir.iterdir():
+        if not path.is_dir():
+            continue
+        try:
+            value = float(path.name)
+        except ValueError:
+            continue
+        if value > 0:
+            values.append((value, path))
+    if values:
+        latest = max(value for value, _ in values)
+        return latest, [path for value, path in values if value == latest], "reconstructed"
+    processors = sorted(
+        (path for path in case_dir.iterdir() if path.is_dir() and re.fullmatch(r"processor\d+", path.name)),
+        key=lambda path: int(path.name[9:]),
+    )
+    processor_times = []
+    for processor in processors:
+        found = []
+        for path in processor.iterdir():
+            if not path.is_dir():
+                continue
+            try:
+                value = float(path.name)
+            except ValueError:
+                continue
+            if value > 0:
+                found.append((value, path))
+        processor_times.append(sorted(found))
+    if processors and all(processor_times):
+        common = set(value for value, _ in processor_times[0])
+        for values in processor_times[1:]:
+            common.intersection_update(value for value, _ in values)
+        if not common:
+            return None, [], "missing"
+        latest = max(common)
+        selected = [
+            next(path for value, path in values if value == latest)
+            for values in processor_times
+        ]
+        return latest, selected, "decomposed"
+    return None, [], "missing"
+
+
+def latest_time_dir(case_dir: Path | None) -> tuple[float | None, Path | None]:
+    latest, directories, _ = final_time_dirs(case_dir)
+    return latest, directories[0] if directories else None
+
+
+def read_logs(paths: tuple[Path, ...] | list[Path]) -> str:
+    return "\n".join(read_text(path) for path in paths if path.is_file())
+
+
+def normal_end(log_text: str) -> bool:
+    return re.search(r"(?m)^\s*End\s*$", log_text) is not None
+
+
+def converged_early(log_text: str) -> bool:
+    return re.search(r"solution converged|convergence criterion satisfied", log_text, re.I) is not None
+
+
+def final_log_time(log_text: str) -> float | None:
+    values = [float(match.group(1)) for match in TIME_RE.finditer(log_text)]
+    return values[-1] if values else None
diff --git a/benchmarks/evaluation/foam_arrays.py b/benchmarks/evaluation/foam_arrays.py
new file mode 100644
index 0000000000000000000000000000000000000000..a0180f66bf6db8e744b20fa2d9e12a57aef08fee
--- /dev/null
+++ b/benchmarks/evaluation/foam_arrays.py
@@ -0,0 +1,129 @@
+#!/usr/bin/env python3
+"""Read complete OpenFOAM primitive arrays for v3 scientific QoIs."""
+from __future__ import annotations
+
+import gzip
+import re
+import struct
+from pathlib import Path
+from typing import Literal
+
+
+NUMBER = rb"[-+]?(?:\d+\.?\d*|\.\d+)(?:[eE][-+]?\d+)?"
+
+
+class FoamArrayError(RuntimeError):
+    """Raised when a primitive array cannot be decoded unambiguously."""
+
+
+def _bytes(path: Path) -> bytes:
+    return gzip.decompress(path.read_bytes()) if path.suffix == ".gz" else path.read_bytes()
+
+
+def _header(data: bytes) -> bytes:
+    end = data.find(b"// * * *")
+    return data[: end if end >= 0 else min(len(data), 4096)]
+
+
+def _format(data: bytes) -> Literal["ascii", "binary"]:
+    match = re.search(rb"\bformat\s+(ascii|binary)\s*;", _header(data))
+    if not match:
+        raise FoamArrayError("OpenFOAM header has no format entry")
+    return match.group(1).decode("ascii")  # type: ignore[return-value]
+
+
+def _arch(data: bytes) -> tuple[str, int, int]:
+    match = re.search(rb'\barch\s+"([^\"]+)"\s*;', _header(data))
+    arch = match.group(1).decode("ascii") if match else "LSB;label=32;scalar=64"
+    endian = ">" if arch.startswith("MSB") else "<"
+    label = int(re.search(r"label=(32|64)", arch).group(1)) if "label=" in arch else 32
+    scalar = int(re.search(r"scalar=(32|64)", arch).group(1)) if "scalar=" in arch else 64
+    return endian, label, scalar
+
+
+def _list_payload(data: bytes, marker: bytes | None = None) -> tuple[int, bytes]:
+    if marker is None:
+        header_end = data.find(b"// * * *")
+        search = data[header_end if header_end >= 0 else 0 :]
+        match = re.search(rb"\b(\d+)\s*\(", search)
+        offset = (header_end if header_end >= 0 else 0) + (match.end() if match else 0)
+    else:
+        match = re.search(marker + rb"\s+(\d+)\s*\(", data)
+        offset = match.end() if match else 0
+    if not match:
+        raise FoamArrayError("OpenFOAM nonuniform list header was not found")
+    while offset < len(data) and data[offset : offset + 1] in (b"\n", b"\r"):
+        offset += 1
+    return int(match.group(1)), data[offset:]
+
+
+def _ascii_body(payload: bytes) -> bytes:
+    end = payload.rfind(b")")
+    return payload[:end] if end >= 0 else payload
+
+
+def read_scalar_field(path: Path) -> list[float]:
+    data = _bytes(path)
+    uniform = re.search(rb"internalField\s+uniform\s+(" + NUMBER + rb")", data)
+    if uniform:
+        return [float(uniform.group(1))]
+    count, payload = _list_payload(data, rb"internalField\s+nonuniform\s+List<scalar>")
+    if _format(data) == "ascii":
+        values = [float(token) for token in re.findall(NUMBER, _ascii_body(payload))[:count]]
+    else:
+        endian, _, scalar_bits = _arch(data)
+        code = "f" if scalar_bits == 32 else "d"
+        size = scalar_bits // 8
+        values = list(struct.unpack(f"{endian}{count}{code}", payload[: count * size]))
+    if len(values) != count:
+        raise FoamArrayError(f"{path}: declared {count} scalars but decoded {len(values)}")
+    return values
+
+
+def read_vector_field(path: Path) -> list[tuple[float, float, float]]:
+    data = _bytes(path)
+    count, payload = _list_payload(data, rb"internalField\s+nonuniform\s+List<vector>")
+    return _decode_vectors(path, data, count, payload)
+
+
+def read_vector_list(path: Path) -> list[tuple[float, float, float]]:
+    data = _bytes(path)
+    count, payload = _list_payload(data)
+    return _decode_vectors(path, data, count, payload)
+
+
+def _decode_vectors(path: Path, data: bytes, count: int, payload: bytes) -> list[tuple[float, float, float]]:
+    if _format(data) == "ascii":
+        rows = re.findall(rb"\(\s*(" + NUMBER + rb")\s+(" + NUMBER + rb")\s+(" + NUMBER + rb")\s*\)", _ascii_body(payload))
+        values = [(float(x), float(y), float(z)) for x, y, z in rows[:count]]
+    else:
+        endian, _, scalar_bits = _arch(data)
+        code = "f" if scalar_bits == 32 else "d"
+        size = scalar_bits // 8
+        flat = struct.unpack(f"{endian}{count * 3}{code}", payload[: count * 3 * size])
+        values = list(zip(flat[0::3], flat[1::3], flat[2::3]))
+    if len(values) != count:
+        raise FoamArrayError(f"{path}: declared {count} vectors but decoded {len(values)}")
+    return values
+
+
+def read_label_list(path: Path) -> list[int]:
+    data = _bytes(path)
+    count, payload = _list_payload(data)
+    if _format(data) == "ascii":
+        values = [int(token) for token in re.findall(rb"[-+]?\d+", _ascii_body(payload))[:count]]
+    else:
+        endian, label_bits, _ = _arch(data)
+        code = "i" if label_bits == 32 else "q"
+        size = label_bits // 8
+        values = list(struct.unpack(f"{endian}{count}{code}", payload[: count * size]))
+    if len(values) != count:
+        raise FoamArrayError(f"{path}: declared {count} labels but decoded {len(values)}")
+    return values
+
+
+def foam_path(directory: Path, name: str) -> Path | None:
+    for candidate in (directory / name, directory / f"{name}.gz"):
+        if candidate.is_file():
+            return candidate
+    return None
diff --git a/benchmarks/evaluation/foam_field.py b/benchmarks/evaluation/foam_field.py
new file mode 100644
index 0000000000000000000000000000000000000000..6bd6e3602342825656398d87ab353d81ae4005d5
--- /dev/null
+++ b/benchmarks/evaluation/foam_field.py
@@ -0,0 +1,155 @@
+from __future__ import annotations
+
+import gzip
+import math
+import mmap
+import re
+import struct
+from pathlib import Path
+from typing import Any, Iterable
+
+NUMBER = r"[-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?"
+NONFINITE_RE = re.compile(r"(?<![A-Za-z])[-+]?(?:nan|inf(?:inity)?)(?![A-Za-z])", re.I)
+FIELD_CLASS_RE = re.compile(
+    r"\bclass\s+(?P<class>(?:vol|surface|point)(?:Scalar|Vector|SphericalTensor|SymmTensor|Tensor)Field)\s*;"
+)
+FORMAT_RE = re.compile(r"\bformat\s+(?P<format>ascii|binary)\s*;")
+OBJECT_RE = re.compile(r"\bobject\s+(?P<object>[^;\s]+)\s*;")
+LIST_RE = re.compile(
+    rb"nonuniform\s+(?:List<)?(?P<type>scalar|vector|sphericalTensor|symmTensor|tensor|label)>?"
+    rb"\s+(?P<count>\d+)\s*\("
+)
+COMPONENTS = {"scalar": 1, "vector": 3, "sphericalTensor": 1, "symmTensor": 6, "tensor": 9, "label": 1}
+
+
+def _stats(values: Iterable[float]) -> dict[str, Any]:
+    low, high, count, nonfinite = math.inf, -math.inf, 0, 0
+    for value in values:
+        count += 1
+        if math.isfinite(value):
+            low, high = min(low, value), max(high, value)
+        else:
+            nonfinite += 1
+    return {
+        "count": count,
+        "finite": nonfinite == 0,
+        "nonfinite_count": nonfinite,
+        "min": None if low == math.inf else low,
+        "max": None if high == -math.inf else high,
+    }
+
+
+def _binary_list_stats(
+    data: bytes | mmap.mmap,
+    match: re.Match[bytes],
+    width: int,
+    byte_order: str,
+) -> dict[str, Any]:
+    kind = match.group("type").decode("ascii")
+    count = int(match.group("count"))
+    item_count = count * COMPONENTS[kind]
+    start, end = match.end(), match.end() + item_count * width
+    if end > len(data) or not bytes(data[end : min(len(data), end + 16)]).lstrip().startswith(b")"):
+        raise ValueError("binary field list does not match its declaration")
+    unpacked = struct.iter_unpack(byte_order + ("d" if width == 8 else "f"), memoryview(data)[start:end])
+    result = _stats(item[0] for item in unpacked)
+    result.update({"value_type": kind, "element_count": count, "components": COMPONENTS[kind]})
+    return result
+
+
+def _binary_internal_data(
+    data: bytes | mmap.mmap,
+    header: str,
+) -> tuple[list[dict[str, Any]], dict[str, Any] | None]:
+    width_match = re.search(r"scalar=(32|64)", header)
+    preferred = int(width_match.group(1)) // 8 if width_match else 8
+    byte_order = ">" if "MSB" in header else "<"
+    records = []
+    for match in LIST_RE.finditer(data):
+        for width in (preferred, 4 if preferred == 8 else 8):
+            try:
+                record = _binary_list_stats(data, match, width, byte_order)
+                record["offset"] = match.start()
+                records.append(record)
+                break
+            except ValueError:
+                continue
+    internal_marker, boundary_marker = data.find(b"internalField"), data.find(b"boundaryField")
+    internal = next(
+        (record for record in records if record["offset"] > internal_marker and (boundary_marker < 0 or record["offset"] < boundary_marker)),
+        None,
+    )
+    if internal is None and internal_marker >= 0:
+        stop = boundary_marker if boundary_marker > internal_marker else min(len(data), internal_marker + 1024)
+        section = bytes(data[internal_marker:stop]).decode("ascii", errors="ignore")
+        uniform = re.search(rf"internalField\s+uniform\s+(\([^;]+\)|{NUMBER})\s*;", section)
+        if uniform:
+            internal = _stats(float(token) for token in re.findall(NUMBER, uniform.group(1)))
+    return records, internal
+
+
+def _binary_internal(path: Path, header: str) -> tuple[list[dict[str, Any]], dict[str, Any] | None]:
+    if path.suffix == ".gz":
+        with gzip.open(path, "rb") as stream:
+            return _binary_internal_data(stream.read(), header)
+    with path.open("rb") as stream, mmap.mmap(stream.fileno(), 0, access=mmap.ACCESS_READ) as data:
+        return _binary_internal_data(data, header)
+
+
+def _ascii_internal(raw: bytes) -> tuple[list[dict[str, Any]], dict[str, Any] | None, bool]:
+    text = raw.decode("utf-8", errors="replace")
+    marker = text.find("internalField")
+    boundary = text.find("boundaryField", marker + 1) if marker >= 0 else -1
+    section = text[marker : boundary if boundary >= 0 else len(text)] if marker >= 0 else ""
+    uniform = re.search(rf"internalField\s+uniform\s+(\([^;]+\)|{NUMBER})\s*;", section)
+    if uniform:
+        internal = _stats(float(token) for token in re.findall(NUMBER, uniform.group(1)))
+        return [internal], internal, NONFINITE_RE.search(section) is not None
+    listed = re.search(
+        rf"internalField\s+nonuniform\s+(?:List<)?(?P<type>scalar|vector|sphericalTensor|symmTensor|tensor)>?"
+        rf"\s+(?P<count>\d+)\s*\((?P<body>.*?)\)\s*;",
+        section,
+        re.S,
+    )
+    if not listed:
+        return [], None, NONFINITE_RE.search(section) is not None
+    values = [float(token) for token in re.findall(NUMBER, listed.group("body"))]
+    internal = _stats(values)
+    kind, count = listed.group("type"), int(listed.group("count"))
+    internal["count_matches_declaration"] = len(values) == count * COMPONENTS[kind]
+    return [internal], internal, NONFINITE_RE.search(section) is not None
+
+
+def scan_field(path: Path, base: Path | None = None) -> dict[str, Any]:
+    base = base or path.parent
+    try:
+        if path.suffix == ".gz":
+            with gzip.open(path, "rb") as stream:
+                header_bytes = stream.read(4096)
+        else:
+            header_bytes = path.read_bytes()[:4096]
+        header = header_bytes.decode("ascii", errors="ignore")
+        field_class, field_format = FIELD_CLASS_RE.search(header), FORMAT_RE.search(header)
+        if not field_class or not field_format:
+            return {"status": "skip", "reason": "not_a_supported_field", "parse_ok": False}
+        if field_format.group("format") == "binary":
+            records, internal = _binary_internal(path, header)
+            nonfinite = any(not record["finite"] for record in records)
+        else:
+            raw = gzip.open(path, "rb").read() if path.suffix == ".gz" else path.read_bytes()
+            records, internal, marker = _ascii_internal(raw)
+            nonfinite = marker or any(not record["finite"] for record in records)
+        parse_ok = internal is not None and all(record.get("count_matches_declaration", True) for record in records)
+        object_match = OBJECT_RE.search(header)
+        return {
+            "path": str(path.relative_to(base)) if path.is_relative_to(base) else str(path),
+            "status": "pass" if parse_ok and not nonfinite else "fail",
+            "class": field_class.group("class"),
+            "format": field_format.group("format"),
+            "field": object_match.group("object") if object_match else path.name.removesuffix(".gz"),
+            "internal": internal,
+            "finite": not nonfinite,
+            "parse_ok": parse_ok,
+        }
+    except (OSError, ValueError, struct.error) as exc:
+        return {"status": "fail", "finite": False, "parse_ok": False, "error": str(exc)}
diff --git a/benchmarks/evaluation/foam_io.py b/benchmarks/evaluation/foam_io.py
new file mode 100644
index 0000000000000000000000000000000000000000..cf5689bef6386b7dfc49cc87f32daf702baefd8a
--- /dev/null
+++ b/benchmarks/evaluation/foam_io.py
@@ -0,0 +1,29 @@
+"""Small shared OpenFOAM file helpers used by evaluators and CLI extractors."""
+from __future__ import annotations
+
+import gzip
+import math
+from pathlib import Path
+
+
+def read_text(path: Path) -> str:
+    try:
+        if path.suffix == ".gz":
+            with gzip.open(path, "rt", encoding="utf-8", errors="ignore") as stream:
+                return stream.read()
+        return path.read_text(encoding="utf-8", errors="replace")
+    except OSError:
+        return ""
+
+
+def field_path(time_dir: Path | None, name: str) -> Path | None:
+    if time_dir is None:
+        return None
+    for candidate in (time_dir / name, time_dir / f"{name}.gz"):
+        if candidate.is_file():
+            return candidate
+    return None
+
+
+def magnitude(values: list[tuple[float, float, float]]) -> list[float]:
+    return [math.sqrt(x * x + y * y + z * z) for x, y, z in values]
diff --git a/benchmarks/evaluation/frozen_recovery.py b/benchmarks/evaluation/frozen_recovery.py
new file mode 100644
index 0000000000000000000000000000000000000000..c67a791e22c712235340056508057326d1cfdfac
--- /dev/null
+++ b/benchmarks/evaluation/frozen_recovery.py
@@ -0,0 +1,713 @@
+#!/usr/bin/env python3
+"""Deterministic QoI recovery for already-finished Extended FoamBench runs.
+
+This module deliberately has no solver or OpenFOAM command dependency.  It
+reads only the retained case files named by an existing campaign artifact and
+returns a new candidate document in memory.  The command-line driver writes
+the audit products to a separate directory; neither the frozen run nor its
+original QoI document is modified.
+"""
+from __future__ import annotations
+
+import copy
+import gzip
+import hashlib
+import json
+import math
+import re
+from dataclasses import dataclass, field
+from pathlib import Path
+from typing import Any, Iterable
+
+from .comparison import compare_case
+from .extbench import (
+    extract_contract_case,
+    evidence_path,
+    field_dimensions,
+    numeric_time_dirs,
+    profile_event_locations,
+    read_scalar_field_allow_uniform,
+    read_vector_field_allow_uniform,
+    structured_qoi_errors,
+)
+from .foam_arrays import foam_path, read_label_list, read_scalar_field, read_vector_list
+
+
+RECOVERY_VERSION = "foambench.frozen_qoi_recovery.v1"
+
+
+@dataclass
+class RecoveryEvidence:
+    """Values and audit information produced by one recovery branch."""
+
+    values: dict[str, Any] = field(default_factory=dict)
+    evidence: dict[str, list[str]] = field(default_factory=dict)
+    methods: dict[str, str] = field(default_factory=dict)
+    source_times: list[float] = field(default_factory=list)
+    preflight: dict[str, Any] = field(default_factory=dict)
+    reasons: list[str] = field(default_factory=list)
+
+
+def sha256_file(path: Path) -> str:
+    digest = hashlib.sha256()
+    with path.open("rb") as stream:
+        for block in iter(lambda: stream.read(1024 * 1024), b""):
+            digest.update(block)
+    return digest.hexdigest()
+
+
+def _raw_bytes(path: Path) -> bytes:
+    return gzip.decompress(path.read_bytes()) if path.suffix == ".gz" else path.read_bytes()
+
+
+def _text(path: Path) -> str:
+    return _raw_bytes(path).decode("utf-8", errors="ignore")
+
+
+def _named_block(text: str, name: str, start: int = 0) -> str | None:
+    match = re.search(r"(?m)^\s*" + re.escape(name) + r"\s*\{", text[start:])
+    if match is None:
+        return None
+    left = start + match.end()
+    depth, index = 1, left
+    while index < len(text) and depth:
+        char = text[index]
+        if char == "{":
+            depth += 1
+        elif char == "}":
+            depth -= 1
+        index += 1
+    return text[left : index - 1] if depth == 0 else None
+
+
+def _boundary_block(case: Path, patch: str) -> str | None:
+    path = foam_path(case / "constant/polyMesh", "boundary")
+    if path is None:
+        return None
+    text = _text(path)
+    anchor = text.find("object      boundary")
+    return _named_block(text, patch, max(anchor, 0))
+
+
+def _boundary_specs(case: Path) -> dict[str, dict[str, Any]]:
+    path = foam_path(case / "constant/polyMesh", "boundary")
+    if path is None:
+        return {}
+    text = _text(path)
+    anchor = max(text.find("object      boundary"), 0)
+    result: dict[str, dict[str, Any]] = {}
+    names = re.finditer(r"(?m)^\s*([A-Za-z_][A-Za-z0-9_]*)\s*\{", text[anchor:])
+    for match in names:
+        name = match.group(1)
+        block = _named_block(text, name, anchor + match.start())
+        if block is None:
+            continue
+        start_match = re.search(r"\bstartFace\s+([0-9]+)\s*;", block)
+        count_match = re.search(r"\bnFaces\s+([0-9]+)\s*;", block)
+        if start_match and count_match:
+            result[name] = {
+                "start_face": int(start_match.group(1)),
+                "n_faces": int(count_match.group(1)),
+                "type": (re.search(r"\btype\s+([^;\s]+)\s*;", block) or [None, ""])[1],
+            }
+    return result
+
+
+def _face_list(case: Path) -> list[list[int]]:
+    path = foam_path(case / "constant/polyMesh", "faces")
+    if path is None:
+        return []
+    text = _text(path)
+    marker = re.search(r"\bobject\s+faces\s*;.*?\n\s*[0-9]+\s*\(\s*\n", text, re.S)
+    if marker is None:
+        return []
+    body = text[marker.end() :]
+    return [
+        [int(value) for value in match.group(1).split()]
+        for match in re.finditer(r"[0-9]+\(\s*([0-9\s]+)\)", body)
+    ]
+
+
+def _polygon_area(points: list[tuple[float, float, float]], indices: list[int]) -> float:
+    if len(indices) < 3:
+        return 0.0
+    origin = points[indices[0]]
+    area = 0.0
+    for left, right in zip(indices[1:-1], indices[2:]):
+        a = tuple(points[left][axis] - origin[axis] for axis in range(3))
+        b = tuple(points[right][axis] - origin[axis] for axis in range(3))
+        cross = (
+            a[1] * b[2] - a[2] * b[1],
+            a[2] * b[0] - a[0] * b[2],
+            a[0] * b[1] - a[1] * b[0],
+        )
+        area += 0.5 * math.sqrt(sum(value * value for value in cross))
+    return area
+
+
+def _patch_geometry(case: Path, patch: str) -> tuple[list[float], list[int]]:
+    specs = _boundary_specs(case)
+    spec = specs.get(patch)
+    mesh = case / "constant/polyMesh"
+    points_path = foam_path(mesh, "points")
+    owner_path = foam_path(mesh, "owner")
+    if spec is None or points_path is None or owner_path is None:
+        return [], []
+    faces = _face_list(case)
+    points = read_vector_list(points_path)
+    owners = read_label_list(owner_path)
+    start, count = spec["start_face"], spec["n_faces"]
+    if start + count > len(faces) or start + count > len(owners):
+        return [], []
+    areas = [_polygon_area(points, faces[index]) for index in range(start, start + count)]
+    return areas, owners[start : start + count]
+
+
+def _scalar_boundary_values(path: Path, patch: str) -> list[float] | None:
+    """Read one scalar patch's ``value`` entry without trusting field names."""
+    text = _text(path)
+    anchor = text.find("boundaryField")
+    block = _named_block(text, patch, max(anchor, 0))
+    if block is None:
+        return None
+    uniform = re.search(r"\bvalue\s+uniform\s+([-+0-9.eE]+)\s*;", block)
+    if uniform:
+        spec = _boundary_specs(path.parents[2] if len(path.parents) > 2 else path.parent)
+        count = spec.get(patch, {}).get("n_faces", 1)
+        return [float(uniform.group(1))] * int(count or 1)
+    listed = re.search(
+        r"\bvalue\s+nonuniform\s+(?:List<)?scalar>?\s+([0-9]+)\s*\((.*?)\)\s*;",
+        block,
+        re.S,
+    )
+    if listed is None:
+        return None
+    count = int(listed.group(1))
+    values = [float(item) for item in re.findall(r"[-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?", listed.group(2))]
+    return values[:count] if len(values) >= count else None
+
+
+def _field_boundary_scalar(path: Path, patch: str, face_count: int) -> list[float] | None:
+    """Boundary scalar reader with an explicit face count from the mesh."""
+    text = _text(path)
+    anchor = text.find("boundaryField")
+    block = _named_block(text, patch, max(anchor, 0))
+    if block is None:
+        return None
+    uniform = re.search(r"\bvalue\s+uniform\s+([-+0-9.eE]+)\s*;", block)
+    if uniform:
+        return [float(uniform.group(1))] * face_count
+    listed = re.search(
+        r"\bvalue\s+nonuniform\s+(?:List<)?scalar>?\s+([0-9]+)\s*\((.*?)\)\s*;",
+        block,
+        re.S,
+    )
+    if listed is None:
+        return None
+    count = int(listed.group(1))
+    values = [float(item) for item in re.findall(r"[-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?", listed.group(2))]
+    return values[:count] if len(values) >= count else None
+
+
+def _patch_sum_history(case: Path, field: str, patch: str, targets: Iterable[float]) -> tuple[list[dict[str, float]], list[str], list[float], str | None]:
+    specs = _boundary_specs(case)
+    face_count = int(specs.get(patch, {}).get("n_faces", 0))
+    if face_count <= 0:
+        return [], [], [], "patch is absent from boundary contract"
+    target_values = sorted({float(value) for value in targets})
+    dirs = numeric_time_dirs(case)
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    source_times: list[float] = []
+    for target in target_values:
+        nearest = min(dirs, key=lambda item: abs(item[0] - target), default=None)
+        if nearest is None or abs(nearest[0] - target) > 1e-8 * max(1.0, abs(target)):
+            continue
+        actual_time, directory = nearest
+        path = foam_path(directory, field)
+        if path is None:
+            continue
+        values = _field_boundary_scalar(path, patch, face_count)
+        if not values or any(not math.isfinite(value) for value in values):
+            continue
+        points.append({"time": actual_time, "value": float(sum(values))})
+        evidence.append(evidence_path(case, path))
+        source_times.append(actual_time)
+    return points, sorted(set(evidence)), sorted(set(source_times)), None
+
+
+def _patch_average_history(case: Path, field: str, patch: str, targets: Iterable[float]) -> tuple[list[dict[str, float]], list[str], list[float], str | None]:
+    areas, owners = _patch_geometry(case, patch)
+    if not areas or not owners or sum(areas) <= 0:
+        return [], [], [], "patch geometry could not be reconstructed"
+    target_values = sorted({float(value) for value in targets})
+    dirs = numeric_time_dirs(case)
+    points: list[dict[str, float]] = []
+    evidence: list[str] = []
+    source_times: list[float] = []
+    for target in target_values:
+        nearest = min(dirs, key=lambda item: abs(item[0] - target), default=None)
+        if nearest is None or abs(nearest[0] - target) > 1e-8 * max(1.0, abs(target)):
+            continue
+        actual_time, directory = nearest
+        path = foam_path(directory, field)
+        if path is None:
+            continue
+        try:
+            values = read_scalar_field_allow_uniform(path, max(owners) + 1)
+        except (OSError, ValueError, RuntimeError):
+            continue
+        if len(values) <= max(owners):
+            continue
+        total_area = sum(areas)
+        average = sum(area * values[owner] for area, owner in zip(areas, owners)) / total_area
+        if not math.isfinite(average):
+            continue
+        points.append({"time": actual_time, "value": float(average)})
+        evidence.append(evidence_path(case, path))
+        source_times.append(actual_time)
+    return points, sorted(set(evidence)), sorted(set(source_times)), None
+
+
+def _reference_times(reference: dict[str, Any], metric_names: Iterable[str]) -> list[float]:
+    times: set[float] = set()
+    for metric in metric_names:
+        value = reference.get("qois", {}).get(metric)
+        if not isinstance(value, dict):
+            continue
+        if value.get("kind") == "time_history":
+            for point in value.get("points", []):
+                if isinstance(point, dict) and isinstance(point.get("time"), (int, float)):
+                    times.add(float(point["time"]))
+        elif value.get("kind") == "branched_time_histories":
+            for branch in value.get("branches", {}).values():
+                if isinstance(branch, dict):
+                    for point in branch.get("points", []):
+                        if isinstance(point, dict) and isinstance(point.get("time"), (int, float)):
+                            times.add(float(point["time"]))
+    return sorted(times)
+
+
+def _history(quantity: str, points: list[dict[str, float]], dimensions: str | None = None) -> dict[str, Any]:
+    value: dict[str, Any] = {"kind": "time_history", "quantity": quantity, "points": sorted(points, key=lambda item: item["time"])}
+    if dimensions:
+        value["field_dimensions"] = dimensions
+    return value
+
+
+def recover_ercofta(case: Path, reference: dict[str, Any], variant: str) -> RecoveryEvidence:
+    result = RecoveryEvidence()
+    reference_times = _reference_times(reference, ("mass_flow_rate", "pressure_rise"))
+    available_times = [time for time, _ in numeric_time_dirs(case)]
+    expected_latest = max(reference_times, default=None)
+    observed_latest = max(available_times, default=None)
+    result.preflight.update({
+        "reference_latest_time": expected_latest,
+        "retained_latest_time": observed_latest,
+        "time_semantics": "numeric_directory_name_exact_match",
+    })
+    if variant != "1" and expected_latest is not None and (observed_latest is None or observed_latest < expected_latest - 1e-10 * max(1.0, expected_latest)):
+        result.reasons.append(
+            f"retained result ends at {observed_latest!r}, before reference time {expected_latest!r}; no time rescaling is permitted"
+        )
+        result.preflight["status"] = "fail"
+        return result
+    mass_points, mass_refs, mass_times, mass_error = _patch_sum_history(case, "phi", "inlet", reference_times)
+    pressure_points_in, pressure_refs_in, pressure_times_in, pressure_error_in = _patch_average_history(case, "p", "inlet", reference_times)
+    pressure_points_out, pressure_refs_out, pressure_times_out, pressure_error_out = _patch_average_history(case, "p", "outlet", reference_times)
+    result.preflight.update({
+        "status": "pass" if mass_points or pressure_points_in else "fail",
+        "mass_point_count": len(mass_points),
+        "pressure_inlet_point_count": len(pressure_points_in),
+        "pressure_outlet_point_count": len(pressure_points_out),
+    })
+    if mass_points:
+        result.values["mass_flow_rate"] = _history("explicit_mass_flow", mass_points, field_dimensions(case, "phi"))
+        result.evidence["mass_flow_rate"] = mass_refs
+        result.methods["mass_flow_rate"] = "retained_phi_boundary_sum.v1"
+        result.source_times.extend(mass_times)
+    if pressure_points_in and pressure_points_out:
+        inlet = {round(point["time"], 12): point["value"] for point in pressure_points_in}
+        outlet = {round(point["time"], 12): point["value"] for point in pressure_points_out}
+        points = [{"time": time, "value": outlet[time] - inlet[time]} for time in sorted(set(inlet) & set(outlet))]
+        if points:
+            result.values["pressure_rise"] = {
+                "kind": "time_history",
+                "quantity": "pressure_rise",
+                "definition": "outlet_minus_inlet_patch_owner_cell_area_average",
+                "source_patches": {"inlet": "inlet", "outlet": "outlet"},
+                "points": points,
+            }
+            result.evidence["pressure_rise"] = sorted(set(pressure_refs_in + pressure_refs_out))
+            result.methods["pressure_rise"] = "retained_p_owner_cell_patch_area_average.v1"
+            result.source_times.extend(pressure_times_in + pressure_times_out)
+    for error in (mass_error, pressure_error_in, pressure_error_out):
+        if error:
+            result.reasons.append(error)
+    if expected_latest is not None and not mass_points and not pressure_points_in:
+        result.reasons.append(
+            "no retained time directory matches the reference time grid; time units or scale are not inferred"
+        )
+    result.source_times = sorted(set(result.source_times))
+    return result
+
+
+def _case_branch_dirs(case: Path) -> dict[str, Path]:
+    parent = case.parent
+    result = {"pBack_101325": case}
+    for path in parent.glob("case_pBack_*"):
+        match = re.fullmatch(r"case_pBack_([0-9]+)", path.name)
+        if match and path.is_dir():
+            result[f"pBack_{match.group(1)}"] = path
+    return result
+
+
+def recover_nozzle(case: Path, reference: dict[str, Any], adapter: str, variant: str) -> RecoveryEvidence:
+    result = RecoveryEvidence()
+    reference_value = reference.get("qois", {}).get("mass_flow_rate", {})
+    if variant == "4" and adapter == "easyfoam" and reference_value.get("kind") == "branched_time_histories":
+        branches: dict[str, Any] = {}
+        evidence: list[str] = []
+        sources: dict[str, float] = {}
+        for branch, history in reference_value.get("branches", {}).items():
+            branch_case = _case_branch_dirs(case).get(branch)
+            points = history.get("points", []) if isinstance(history, dict) else []
+            target = [point.get("time") for point in points if isinstance(point, dict) and isinstance(point.get("time"), (int, float))]
+            if branch_case is None or not target:
+                result.reasons.append(f"missing retained branch directory or target time for {branch}")
+                continue
+            branch_points, refs, times, error = _patch_sum_history(branch_case, "phi", "inlet", target)
+            if branch_points:
+                branches[branch] = _history("explicit_mass_flow", branch_points, field_dimensions(branch_case, "phi"))
+                # ``evidence_path`` is relative to each branch case.  Add the
+                # sibling directory explicitly so three otherwise identical
+                # ``0.005/phi`` paths cannot be confused in the manifest.
+                if branch_case != case:
+                    evidence.extend(f"../{branch_case.name}/{ref}" for ref in refs)
+                else:
+                    evidence.extend(refs)
+                if times:
+                    sources[branch] = max(times)
+            elif error:
+                result.reasons.append(f"{branch}: {error}")
+        if branches:
+            result.values["mass_flow_rate"] = {
+                "kind": "branched_time_histories",
+                "quantity": "explicit_mass_flow",
+                "field_dimensions": field_dimensions(case, "phi"),
+                "branches": branches,
+            }
+            result.evidence["mass_flow_rate"] = sorted(set(evidence))
+            result.methods["mass_flow_rate"] = "retained_branch_phi_boundary_sum.v1"
+            result.preflight.update({"status": "pass", "branches": sorted(branches), "source_times": sources})
+            result.source_times.extend(sources.values())
+        else:
+            result.preflight["status"] = "fail"
+        return result
+    if variant == "2" and adapter == "foamagent" and reference_value.get("kind") == "time_history":
+        targets = [point.get("time") for point in reference_value.get("points", []) if isinstance(point, dict) and isinstance(point.get("time"), (int, float))]
+        points, refs, times, error = _patch_sum_history(case, "phi", "inlet", targets)
+        if points:
+            result.values["mass_flow_rate"] = _history("explicit_mass_flow", points, field_dimensions(case, "phi"))
+            result.evidence["mass_flow_rate"] = refs
+            result.methods["mass_flow_rate"] = "retained_phi_boundary_sum.v1"
+            result.source_times.extend(times)
+            result.preflight.update({"status": "pass", "point_count": len(points), "source_times": times})
+        else:
+            result.preflight["status"] = "fail"
+            if error:
+                result.reasons.append(error)
+        return result
+    result.preflight["status"] = "not_applicable"
+    return result
+
+
+def _final_fields(case: Path) -> tuple[float, Path] | None:
+    for time, directory in reversed(numeric_time_dirs(case)):
+        if all(foam_path(directory, name) is not None for name in ("C", "U", "rho", "p", "T")):
+            return time, directory
+    return None
+
+
+def recover_riemann(case: Path) -> RecoveryEvidence:
+    result = RecoveryEvidence()
+    final = _final_fields(case)
+    if final is None:
+        result.preflight = {"status": "fail", "reason": "final C/U/rho/p/T fields are not all retained"}
+        return result
+    time, directory = final
+    try:
+        centres = read_vector_list(foam_path(directory, "C"))  # type: ignore[arg-type]
+        velocity = read_vector_field_allow_uniform(foam_path(directory, "U"), len(centres))  # type: ignore[arg-type]
+        rho = read_scalar_field_allow_uniform(foam_path(directory, "rho"), len(centres))  # type: ignore[arg-type]
+        pressure = read_scalar_field_allow_uniform(foam_path(directory, "p"), len(centres))  # type: ignore[arg-type]
+        temperature = read_scalar_field_allow_uniform(foam_path(directory, "T"), len(centres))  # type: ignore[arg-type]
+    except (OSError, ValueError, RuntimeError) as exc:
+        result.preflight = {"status": "fail", "reason": f"field decoding failed: {exc}"}
+        return result
+    if not all(len(values) == len(centres) for values in (velocity, rho, pressure, temperature)):
+        result.preflight = {"status": "fail", "reason": "final fields have inconsistent cell counts"}
+        return result
+    x_target = min((point[0] for point in centres), key=lambda value: abs(value))
+    y_target = min((point[1] for point in centres), key=lambda value: abs(value))
+    horizontal_indices = [index for index, point in enumerate(centres) if abs(point[1] - y_target) <= 1e-10 * max(1.0, abs(y_target))]
+    vertical_indices = [index for index, point in enumerate(centres) if abs(point[0] - x_target) <= 1e-10 * max(1.0, abs(x_target))]
+    horizontal_indices.sort(key=lambda index: centres[index][0])
+    vertical_indices.sort(key=lambda index: centres[index][1])
+    columns_h = ["x", "rho", "U_x", "U_y", "U_z", "p", "T"]
+    columns_v = ["y", "rho", "U_x", "U_y", "U_z", "p", "T"]
+    rows_h = [[centres[i][0], rho[i], *velocity[i], pressure[i], temperature[i]] for i in horizontal_indices]
+    rows_v = [[centres[i][1], rho[i], *velocity[i], pressure[i], temperature[i]] for i in vertical_indices]
+    if len(rows_h) < 5 or len(rows_v) < 5:
+        result.preflight = {"status": "fail", "reason": "centerline preflight retained fewer than five cells", "horizontal_count": len(rows_h), "vertical_count": len(rows_v)}
+        return result
+    root = evidence_path(case, directory / "C")
+    refs = sorted({root, evidence_path(case, directory / "U"), evidence_path(case, directory / "rho"), evidence_path(case, directory / "p"), evidence_path(case, directory / "T")})
+    profiles = {
+        "kind": "named_profiles",
+        "profiles": [
+            {"profile_id": f"recovery/{time:g}/horizontal.xy", "columns": columns_h, "rows": rows_h},
+            {"profile_id": f"recovery/{time:g}/vertical.xy", "columns": columns_v, "rows": rows_v},
+        ],
+    }
+    result.values["centerline_profiles"] = profiles
+    result.values["event_locations"] = profile_event_locations(profiles)
+    result.evidence["centerline_profiles"] = refs
+    result.evidence["event_locations"] = refs
+    result.methods["centerline_profiles"] = "retained_final_cell_centerline_sampling.v1"
+    result.methods["event_locations"] = "retained_final_cell_centerline_sampling_gradient_peaks.v1"
+    result.source_times = [time]
+    result.preflight = {
+        "status": "pass",
+        "source_time": time,
+        "horizontal_cell_count": len(rows_h),
+        "vertical_cell_count": len(rows_v),
+        "selected_coordinates": {"x": x_target, "y": y_target},
+    }
+    if result.values["event_locations"] is None:
+        result.values.pop("event_locations", None)
+        result.evidence.pop("event_locations", None)
+        result.methods.pop("event_locations", None)
+        result.reasons.append("centerline profiles were available but no local pressure/rho gradient event was detected")
+    return result
+
+
+def _nu_value(case: Path) -> tuple[float | None, str | None]:
+    for path in (case / "constant/physicalProperties", case / "constant/transportProperties", case / "constant/thermophysicalProperties"):
+        if not path.is_file():
+            continue
+        match = re.search(r"(?m)^\s*nu\s+(?:\[[^]]+\]\s*)?([-+0-9.eE]+)\s*;", _text(path))
+        if match:
+            return float(match.group(1)), evidence_path(case, path)
+    return None, None
+
+
+def _vector_boundary_uniform(path: Path, patch: str) -> tuple[float, float, float] | None:
+    text = _text(path)
+    anchor = text.find("boundaryField")
+    block = _named_block(text, patch, max(anchor, 0))
+    if block is None:
+        return None
+    match = re.search(r"\bvalue\s+uniform\s*\(\s*([-+0-9.eE]+)\s+([-+0-9.eE]+)\s+([-+0-9.eE]+)\s*\)\s*;", block)
+    return tuple(float(match.group(index)) for index in range(1, 4)) if match else None
+
+
+def _first_cell_distance(case: Path) -> tuple[float | None, str | None]:
+    candidates = sorted(case.glob("postProcessing/wallLawSets/*/yLine.csv"))
+    for path in reversed(candidates):
+        rows = []
+        try:
+            for line in path.read_text(encoding="utf-8", errors="ignore").splitlines()[1:]:
+                parts = [float(item) for item in line.split(",")]
+                if len(parts) >= 2:
+                    rows.append(abs(parts[1]))
+        except (OSError, ValueError):
+            continue
+        positive = [value for value in rows if value > 0 and math.isfinite(value)]
+        if positive:
+            return min(positive), evidence_path(case, path)
+    return None, None
+
+
+def recover_yplus(case: Path) -> RecoveryEvidence:
+    result = RecoveryEvidence()
+    final = next(((time, directory) for time, directory in reversed(numeric_time_dirs(case)) if foam_path(directory, "wallShearStress")), None)
+    nu, nu_ref = _nu_value(case)
+    distance, distance_ref = _first_cell_distance(case)
+    if final is None or nu is None or distance is None:
+        result.preflight = {"status": "fail", "final_wall_shear": bool(final), "nu": nu, "first_cell_distance": distance}
+        result.reasons.append("wall shear, kinematic viscosity, or first-cell distance is absent")
+        return result
+    time, directory = final
+    wall_patches = [name for name, spec in _boundary_specs(case).items() if str(spec.get("type")) == "wall"]
+    values: list[float] = []
+    shear_path = foam_path(directory, "wallShearStress")
+    for patch in wall_patches:
+        vector = _vector_boundary_uniform(shear_path, patch) if shear_path else None
+        if vector is not None:
+            values.append(math.sqrt(sum(component * component for component in vector)))
+    if not values:
+        result.preflight = {"status": "fail", "reason": "wallShearStress has no parseable wall patch value"}
+        return result
+    tau = statistics_mean(values)
+    yplus = math.sqrt(max(tau, 0.0)) * distance / nu
+    if not math.isfinite(yplus):
+        result.preflight = {"status": "fail", "reason": "derived y+ is non-finite"}
+        return result
+    refs = [evidence_path(case, shear_path)] if shear_path else []
+    refs.extend(item for item in (nu_ref, distance_ref) if item)
+    result.values["first_cell_yplus"] = float(yplus)
+    result.evidence["first_cell_yplus"] = sorted(set(refs))
+    result.methods["first_cell_yplus"] = "retained_wall_shear_first_cell_distance.v1"
+    result.source_times = [time]
+    result.preflight = {"status": "pass", "source_time": time, "wall_patch_count": len(values), "tau_magnitude": tau, "nu": nu, "first_cell_distance": distance}
+    result.reasons.append("derived endpoint is an auditable wall-shear estimate, not a substituted Spalding profile")
+    return result
+
+
+def statistics_mean(values: list[float]) -> float:
+    return sum(values) / len(values) if values else math.nan
+
+
+def _merge_candidate(candidate: dict[str, Any], recovery: RecoveryEvidence) -> dict[str, Any]:
+    result = copy.deepcopy(candidate)
+    qois = result.setdefault("qois", {})
+    evidence = result.setdefault("evidence", {})
+    methods = result.setdefault("metric_methods", {})
+    resolver = result.setdefault("resolver_report", {})
+    for metric, value in recovery.values.items():
+        qois[metric] = value
+        evidence[metric] = sorted(set(recovery.evidence.get(metric, [])))
+        methods[metric] = recovery.methods.get(metric, "frozen_recovery.v1")
+        resolver[metric] = {
+            "status": "selected",
+            "selected_evidence": evidence[metric],
+            "method": methods[metric],
+            "physical_validation": "metric_extractor_contract.v1",
+        }
+    required = list(result.get("required_metrics", []))
+    missing = sorted(set(required) - set(qois))
+    result["missing_metrics"] = missing
+    result["status"] = "complete" if not missing and not result.get("extraction_errors") else "incomplete"
+    health = result.setdefault("health", {})
+    checks = health.setdefault("checks", {})
+    checks["principal_qoi_complete"] = not missing
+    checks["principal_extraction_error_free"] = not result.get("extraction_errors")
+    validation_errors = [
+        error for name, value in qois.items() if name in required for error in structured_qoi_errors(name, value)
+    ]
+    checks["structured_qoi_valid"] = not validation_errors
+    health["status"] = "pass" if not missing and not validation_errors and not result.get("extraction_errors") else "incomplete"
+    health["validation_errors"] = validation_errors + list(result.get("extraction_errors", []))
+    return result
+
+
+def recover_case(
+    case_id: str,
+    case: Path,
+    reference: dict[str, Any],
+    *,
+    adapter: str,
+    design: dict[str, Any],
+) -> dict[str, Any]:
+    """Re-extract and, where justified, recover one selected incomplete case."""
+    original = extract_contract_case(case, case_id, design)
+    original_comparison = compare_case(reference, original, 1.0)
+    family, variant = case_id.split("/", 1)
+    recovery = RecoveryEvidence(preflight={"status": "not_applicable"})
+    if family == "ERCOFTA_pump":
+        recovery = recover_ercofta(case, reference, variant)
+    elif family == "nozzleCDV":
+        recovery = recover_nozzle(case, reference, adapter, variant)
+    elif family == "riemann2D":
+        recovery = recover_riemann(case)
+    elif family == "yPlusVerification" and variant == "1" and adapter == "easyfoam":
+        recovery = recover_yplus(case)
+    elif family == "supersonicCrossJet" and variant == "1":
+        recovery.reasons.append("declared interior pressure window contains no valid retained cell; global extrema are not an allowed proxy")
+        recovery.preflight = {"status": "fail", "check": "declared_internal_window_nonempty", "observed_cell_count": 0}
+    merged = _merge_candidate(original, recovery)
+    comparison = compare_case(reference, merged, 1.0)
+    if "incomplete" in str(comparison.get("status")):
+        recovery_status = "irrecoverable_incomplete"
+    elif comparison.get("status") == "out_of_tolerance":
+        recovery_status = "recovered_out_of_tolerance"
+    elif comparison.get("status") == "pass":
+        recovery_status = "recovered_complete"
+    else:
+        recovery_status = "recovery_evaluation_error"
+    return {
+        "case_id": case_id,
+        "family": family,
+        "variant": variant,
+        "case_dir": str(case.resolve()),
+        "original": {
+            "reextract_status": original_comparison.get("status"),
+            "reextract_missing_metrics": original_comparison.get("missing_metrics", []),
+            "reextract_out_of_tolerance_metrics": original_comparison.get("out_of_tolerance_metrics", []),
+            "reextract_candidate_missing_metrics": original.get("missing_metrics", []),
+        },
+        "recovery": {
+            "status": recovery_status,
+            "version": RECOVERY_VERSION,
+            "methods": recovery.methods,
+            "source_evidence": recovery.evidence,
+            "source_times": recovery.source_times,
+            "preflight": recovery.preflight,
+            "reasons": recovery.reasons,
+        },
+        "candidate": merged,
+        "comparison": comparison,
+    }
+
+
+def recovery_score_record(source: dict[str, Any], recovered: dict[str, Any]) -> dict[str, Any]:
+    """Build a compact campaign-compatible record without rerunning checks."""
+    original = source
+    comparison = recovered["comparison"]
+    execution = copy.deepcopy(original.get("execution", {}))
+    numerical = copy.deepcopy(original.get("numerical", {}))
+    execution_pass = execution.get("status") == "pass"
+    numerical_pass = numerical.get("status") == "pass" or bool(numerical.get("pass"))
+    qoi_pass = bool(comparison.get("physics_grounded_qoi_pass"))
+    failure_categories: list[str] = []
+    if not execution_pass:
+        failure_categories.append("execution_failure")
+    elif "incomplete" in str(comparison.get("status", "")):
+        failure_categories.append("qoi_incomplete")
+    elif comparison.get("status") == "out_of_tolerance":
+        failure_categories.append("qoi_out_of_tolerance")
+    return {
+        "schema_version": "foambench.frozen_case_recovery.v1",
+        "case_id": recovered["case_id"],
+        "dataset": original.get("dataset", "extended"),
+        "family": recovered["family"],
+        "variant": recovered["variant"],
+        "replicate": original.get("replicate", 1),
+        "artifact": {
+            "case_dir": recovered["case_dir"],
+            "rollout_dir": original.get("artifact", {}).get("rollout_dir"),
+            "workspace_dir": original.get("artifact", {}).get("workspace_dir"),
+        },
+        "execution": execution,
+        "numerical": numerical,
+        "qoi": {
+            "status": "pass" if qoi_pass else comparison.get("status", "evaluation_error"),
+            "physics_grounded_qoi_pass": qoi_pass,
+            "effective_pass_ratio": float(comparison.get("qoi_pass_ratio", 0.0) or 0.0),
+            "candidate": recovered["candidate"],
+            "comparison": comparison,
+        },
+        "scores": {
+            "execution_pass": execution_pass,
+            "numerical_pass": numerical_pass,
+            "physics_grounded_qoi_pass": qoi_pass,
+            "end_to_end_pass": execution_pass and numerical_pass and qoi_pass,
+        },
+        "failure_categories": failure_categories,
+        "recovery": recovered["recovery"],
+    }
+
+
+def document_checksum(path: Path) -> dict[str, Any]:
+    return {"path": str(path.resolve()), "sha256": sha256_file(path), "size_bytes": path.stat().st_size}
diff --git a/benchmarks/evaluation/health.py b/benchmarks/evaluation/health.py
new file mode 100644
index 0000000000000000000000000000000000000000..6829c3425d572d22ce9be682511d7db6079cae8e
--- /dev/null
+++ b/benchmarks/evaluation/health.py
@@ -0,0 +1,69 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from .foam import final_time_dirs
+from .foam_field import scan_field
+from .foam_io import field_path
+
+SCALAR_FIELDS = (
+    "p", "p_rgh", "T", "rho", "nut", "k", "epsilon", "omega", "nuTilda",
+    "Qdot", "CH4", "O2", "CO2", "H2O", "N2", "alpha.water", "alpha.air",
+    "h", "hTotal",
+)
+POSITIVE_FIELDS = {"T", "rho", "k", "epsilon", "omega", "nuTilda", "h", "hTotal"}
+
+
+def final_field_health(case_dir: Path | None) -> dict[str, Any]:
+    latest, time_dirs, layout = final_time_dirs(case_dir)
+    if not time_dirs:
+        return {
+            "status": "unavailable",
+            "latest_time": latest,
+            "checks": {},
+            "reason": "no_final_time_directory",
+        }
+    parsed: list[str] = []
+    nonfinite: list[str] = []
+    bound_failures: list[str] = []
+    parse_errors: dict[str, str] = {}
+    bounds: dict[str, dict[str, float]] = {}
+    for name in SCALAR_FIELDS:
+        paths = [path for time_dir in time_dirs for path in [field_path(time_dir, name)] if path is not None]
+        if not paths:
+            continue
+        records = [scan_field(path, case_dir) for path in paths]
+        invalid = [record for record in records if not record.get("parse_ok")]
+        if invalid:
+            parse_errors[name] = str(invalid[0].get("error") or invalid[0].get("reason") or "internalField is not parseable")
+            continue
+        if any(not record.get("finite") for record in records):
+            nonfinite.append(name)
+        extrema = [record.get("internal") for record in records]
+        lows = [float(item["min"]) for item in extrema if isinstance(item, dict) and isinstance(item.get("min"), (int, float))]
+        highs = [float(item["max"]) for item in extrema if isinstance(item, dict) and isinstance(item.get("max"), (int, float))]
+        if not lows or not highs:
+            continue
+        parsed.append(name)
+        low, high = min(lows), max(highs)
+        bounds[name] = {"min": low, "max": high}
+        if name in POSITIVE_FIELDS and low < -1e-12:
+            bound_failures.append(name)
+        if name.startswith("alpha.") and (low < -1e-3 or high > 1.0 + 1e-3):
+            bound_failures.append(f"{name}_bounds")
+    checks = {
+        "parsed_fields_finite": not nonfinite and not parse_errors,
+        "applicable_field_bounds_valid": not bound_failures,
+    }
+    return {
+        "status": "pass" if all(checks.values()) else "fail",
+        "latest_time": latest,
+        "layout": layout,
+        "checks": checks,
+        "parsed_fields": sorted(parsed),
+        "nonfinite_fields": sorted(nonfinite),
+        "field_bound_failures": sorted(bound_failures),
+        "parse_errors": parse_errors,
+        "bounds": bounds,
+    }
diff --git a/benchmarks/evaluation/io.py b/benchmarks/evaluation/io.py
new file mode 100644
index 0000000000000000000000000000000000000000..58bbfc60dae8b33faa6b1261176e8ccd0004aaa4
--- /dev/null
+++ b/benchmarks/evaluation/io.py
@@ -0,0 +1,39 @@
+from __future__ import annotations
+
+import json
+import math
+from datetime import datetime, timezone
+from pathlib import Path
+from typing import Any
+
+
+def utc_now() -> str:
+    return datetime.now(timezone.utc).isoformat()
+
+
+def read_json(path: Path) -> Any:
+    return json.loads(path.read_text(encoding="utf-8"))
+
+
+def read_object(path: Path) -> dict[str, Any]:
+    value = read_json(path)
+    if not isinstance(value, dict):
+        raise ValueError(f"expected JSON object: {path}")
+    return value
+
+
+def write_json(path: Path, value: Any) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    temporary.write_text(
+        json.dumps(value, ensure_ascii=False, indent=2, sort_keys=True) + "\n",
+        encoding="utf-8",
+    )
+    temporary.replace(path)
+
+
+def finite(value: Any) -> float | None:
+    if isinstance(value, bool) or not isinstance(value, (int, float)):
+        return None
+    number = float(value)
+    return number if math.isfinite(number) else None
diff --git a/benchmarks/evaluation/measurement_specs.py b/benchmarks/evaluation/measurement_specs.py
new file mode 100644
index 0000000000000000000000000000000000000000..f3366e83fc6d289d6995f3f41a21e5391e1e5117
--- /dev/null
+++ b/benchmarks/evaluation/measurement_specs.py
@@ -0,0 +1,45 @@
+"""Load the visible, reference-free Extended measurement contract."""
+from __future__ import annotations
+
+import hashlib
+import json
+from pathlib import Path
+from typing import Any
+
+ROOT = Path(__file__).resolve().parents[2]
+PATH = ROOT / "benchmarks/FoamBench_extended_openfoam13_measurement_specs.json"
+SCHEMA = "easyfoam.extbench.measurement.v1"
+
+
+def _sha(text: str) -> str:
+    return hashlib.sha256(text.encode()).hexdigest()
+
+
+def load_measurement_spec(case_id: str, requirement: str | None = None) -> dict[str, Any] | None:
+    """Return one case contract; reference values and tolerances are absent by construction."""
+    if not PATH.is_file() or "/" not in case_id:
+        return None
+    document = json.loads(PATH.read_text(encoding="utf-8"))
+    if document.get("schema_version") != "easyfoam.extbench.measurement_specs.v1":
+        raise ValueError("unsupported measurement contract")
+    spec = document.get("cases", {}).get(case_id)
+    if not isinstance(spec, dict):
+        return None
+    if spec.get("measurement_schema") != SCHEMA:
+        raise ValueError(f"invalid measurement schema for {case_id}")
+    if requirement is not None:
+        spec = dict(spec)
+        spec["requirement_sha256"] = _sha(requirement)
+    return spec
+
+
+def prompt_measurement_spec(case_id: str, requirement: str) -> str:
+    spec = load_measurement_spec(case_id, requirement)
+    if spec is None:
+        return ""
+    return (
+        "Measurement contract for this ExtBench task (visible task definition; it contains no reference answer or tolerance):\n"
+        + json.dumps(spec, ensure_ascii=False, indent=2)
+        + "\nUse this contract to plan what fields, patches, probes, meshes, and saved times must be retained. "
+        "Do not invent a proxy when a principal measurement is unavailable; report the missing evidence.\n\n"
+    )
diff --git a/benchmarks/evaluation/mesh.py b/benchmarks/evaluation/mesh.py
new file mode 100644
index 0000000000000000000000000000000000000000..29f46f4f3dac0e698ea6f4c50ed96c7443403302
--- /dev/null
+++ b/benchmarks/evaluation/mesh.py
@@ -0,0 +1,54 @@
+from __future__ import annotations
+
+import re
+import subprocess
+from pathlib import Path
+from typing import Any
+
+from .foam import FATAL_RE, NUMBER, read_text
+
+
+def parse_mesh_log(text: str, *, source: str) -> dict[str, Any]:
+    failed_values = [int(value) for value in re.findall(r"Failed\s+(\d+)\s+mesh checks", text, re.I)]
+    min_volumes = [float(value) for value in re.findall(rf"Min volume\s*=\s*({NUMBER})", text)]
+    markers = {
+        "fatal": FATAL_RE.search(text) is not None,
+        "non_positive_cell_volume": min(min_volumes, default=float("inf")) <= 0,
+        "negative_or_zero_volume": re.search(r"(?:negative|zero)\s+(?:cell\s+)?volumes?", text, re.I) is not None,
+        "illegal_face": re.search(r"illegal\s+faces?", text, re.I) is not None,
+        "open_cell": re.search(r"open\s+cells?", text, re.I) is not None,
+        "non_manifold": re.search(r"non[- ]manifold", text, re.I) is not None,
+    }
+    available = "Mesh OK." in text or bool(failed_values) or bool(min_volumes)
+    hard_failure = any(markers.values()) or max(failed_values, default=0) > 0
+    return {
+        "status": "unavailable" if not available else "fail" if hard_failure else "pass",
+        "source": source,
+        "failed_mesh_checks": max(failed_values, default=0),
+        "min_volume": min(min_volumes) if min_volumes else None,
+        "critical_markers": markers,
+    }
+
+
+def mesh_evidence(log_paths: tuple[Path, ...]) -> dict[str, Any]:
+    selected = [
+        path for path in log_paths
+        if "checkmesh" in path.name.lower() or "checkMesh" in read_text(path)[:4096]
+    ]
+    text = "\n".join(read_text(path) for path in selected)
+    return parse_mesh_log(text, source=",".join(str(path) for path in selected))
+
+
+def run_check_mesh(case_dir: Path | None, timeout: float = 120.0) -> dict[str, Any]:
+    if case_dir is None:
+        return {"status": "unavailable", "source": "read_only_replay", "reason": "case_directory_missing"}
+    command = ["checkMesh", "-case", str(case_dir), "-allTopology", "-allGeometry", "-noFunctionObjects"]
+    try:
+        completed = subprocess.run(command, capture_output=True, text=True, check=False, timeout=timeout)
+    except (OSError, subprocess.TimeoutExpired) as exc:
+        return {"status": "fail", "source": "read_only_replay", "command": command, "error": str(exc)}
+    result = parse_mesh_log(completed.stdout + "\n" + completed.stderr, source="read_only_replay")
+    result.update({"command": command, "return_code": completed.returncode})
+    if completed.returncode != 0:
+        result["status"] = "fail"
+    return result
diff --git a/benchmarks/evaluation/models.py b/benchmarks/evaluation/models.py
new file mode 100644
index 0000000000000000000000000000000000000000..c9e1bf9d512385515fdb78b08972a7e07d3bb231
--- /dev/null
+++ b/benchmarks/evaluation/models.py
@@ -0,0 +1,86 @@
+from __future__ import annotations
+
+from dataclasses import dataclass, field
+from pathlib import Path
+from typing import Any
+
+from .io import read_object
+
+
+@dataclass(frozen=True)
+class BenchmarkProfile:
+    profile_id: str
+    dataset: str
+    benchmark_path: Path
+    reference_qois_path: Path
+    expected_case_count: int
+    case_id_style: str = "family_variant"
+    extractor: str = "field"
+    required_qoi_fraction: float = 1.0
+    reference_run_root: Path | None = None
+    numerical_contract: dict[str, Any] = field(default_factory=dict)
+
+    @classmethod
+    def load(cls, path: Path, *, repository_root: Path | None = None) -> "BenchmarkProfile":
+        path = path.resolve(strict=True)
+        data = read_object(path)
+        if repository_root:
+            root = repository_root.resolve()
+        else:
+            root = next(
+                (parent for parent in path.parents if (parent / "benchmarks").is_dir() and (parent / "schemas").is_dir()),
+                path.parent,
+            )
+
+        def resolve(value: str | None) -> Path | None:
+            if value is None:
+                return None
+            candidate = Path(value)
+            return candidate.resolve() if candidate.is_absolute() else (root / candidate).resolve()
+
+        membership = data.get("membership", {})
+        qoi = data.get("qoi", {})
+        return cls(
+            profile_id=str(data["profile_id"]),
+            dataset=str(data["dataset"]),
+            benchmark_path=resolve(str(data["benchmark_path"])),  # type: ignore[arg-type]
+            reference_qois_path=resolve(str(data["reference_qois_path"])),  # type: ignore[arg-type]
+            expected_case_count=int(membership["expected_case_count"]),
+            case_id_style=str(membership.get("case_id_style", "family_variant")),
+            extractor=str(qoi.get("extractor", "field")),
+            required_qoi_fraction=float(qoi.get("required_fraction", 1.0)),
+            reference_run_root=resolve(data.get("reference_run_root")),
+            numerical_contract=dict(data.get("numerical", {})),
+        )
+
+    def identity(self, case_id: str) -> tuple[str, str]:
+        if "/" in case_id:
+            return tuple(case_id.split("/", 1))  # type: ignore[return-value]
+        return case_id, "1"
+
+
+@dataclass(frozen=True)
+class CaseArtifact:
+    case_id: str
+    dataset: str
+    family: str
+    variant: str
+    replicate: int
+    rollout_dir: Path
+    case_dir: Path | None
+    workspace_dir: Path | None = None
+    manifest: dict[str, Any] = field(default_factory=dict)
+    formal_run_records: tuple[Path, ...] = ()
+    solver_logs: tuple[Path, ...] = ()
+    workflow_path: Path | None = None
+    evidence_summary_path: Path | None = None
+
+    @property
+    def duration_seconds(self) -> float | None:
+        value = self.manifest.get("duration_seconds")
+        return float(value) if isinstance(value, (int, float)) else None
+
+    @property
+    def token_usage(self) -> dict[str, Any]:
+        value = self.manifest.get("token_usage")
+        return dict(value) if isinstance(value, dict) else {}
diff --git a/benchmarks/evaluation/numerical.py b/benchmarks/evaluation/numerical.py
new file mode 100644
index 0000000000000000000000000000000000000000..129785cfb619c6d765adfd41db41a744c34ddb3e
--- /dev/null
+++ b/benchmarks/evaluation/numerical.py
@@ -0,0 +1,253 @@
+from __future__ import annotations
+
+import math
+import re
+from pathlib import Path
+from typing import Any
+
+from .foam import FATAL_RE, NONFINITE_RE, NUMBER, final_time_dirs, read_logs
+from .health import final_field_health
+from .mesh import mesh_evidence, run_check_mesh
+from .models import CaseArtifact
+from .stability import numerical_scheme, steady_plateau
+
+RESIDUAL_RE = re.compile(
+    rf"Solving for (?P<field>[^,\r\n]+),\s*Initial residual = (?P<initial>{NUMBER}),\s*Final residual = (?P<final>{NUMBER})"
+)
+COURANT_RE = re.compile(rf"Courant Number mean:\s*(?P<mean>{NUMBER})\s+max:\s*(?P<max>{NUMBER})")
+CONTINUITY_RE = re.compile(
+    rf"(?:time step )?continuity errors\s*:\s*sum local = (?P<local>{NUMBER}),\s*global = (?P<global>{NUMBER}),\s*cumulative = (?P<cumulative>{NUMBER})",
+    re.I,
+)
+
+DEFAULT_CONTRACT = {
+    "final_window_fraction": 0.2,
+    "minimum_final_window_samples": 5,
+    "final_linear_residual": {"reference_factor": 10.0, "absolute_floor": 1e-3},
+    "initial_residual": {"reference_factor": 10.0, "absolute_floor": 1e-3},
+    "courant_final_p95": {"reference_factor": 3.0, "absolute_floor": 1.0},
+    "courant_peak": {"reference_factor": 3.0, "absolute_floor": 2.0},
+    "continuity_global_p95": {"reference_factor": 10.0, "absolute_floor": 1e-5},
+    "continuity_cumulative_final": {"reference_factor": 10.0, "absolute_floor": 1e-3},
+}
+
+
+def percentile(values: list[float], fraction: float) -> float | None:
+    if not values:
+        return None
+    ordered = sorted(values)
+    position = (len(ordered) - 1) * fraction
+    low, high = math.floor(position), math.ceil(position)
+    if low == high:
+        return ordered[low]
+    return ordered[low] + (ordered[high] - ordered[low]) * (position - low)
+
+
+def final_window(values: list[float], contract: dict[str, Any] = DEFAULT_CONTRACT) -> list[float]:
+    count = max(
+        int(contract["minimum_final_window_samples"]),
+        math.ceil(len(values) * float(contract["final_window_fraction"])),
+    )
+    return values[-min(len(values), count):]
+
+
+def parse_logs(paths: list[Path] | tuple[Path, ...], contract: dict[str, Any] = DEFAULT_CONTRACT) -> dict[str, Any]:
+    text = read_logs(paths)
+    residuals: dict[str, dict[str, list[float]]] = {}
+    courants: list[float] = []
+    continuity_global: list[float] = []
+    continuity_cumulative: list[float] = []
+    for match in RESIDUAL_RE.finditer(text):
+        field = match.group("field").strip()
+        values = residuals.setdefault(field, {"initial": [], "final": []})
+        values["initial"].append(float(match.group("initial")))
+        values["final"].append(float(match.group("final")))
+    courants.extend(float(match.group("max")) for match in COURANT_RE.finditer(text))
+    for match in CONTINUITY_RE.finditer(text):
+        continuity_global.append(abs(float(match.group("global"))))
+        continuity_cumulative.append(abs(float(match.group("cumulative"))))
+    residual_summary = {
+        field: {
+            "sample_count": len(values["initial"]),
+            "initial_final_window_p95": percentile(final_window(values["initial"], contract), 0.95),
+            "final_final_window_p95": percentile(final_window(values["final"], contract), 0.95),
+        }
+        for field, values in sorted(residuals.items())
+    }
+    return {
+        "log_paths": [str(path) for path in paths if path.is_file()],
+        "fatal_marker": FATAL_RE.search(text) is not None,
+        "nonfinite_marker": NONFINITE_RE.search(text) is not None,
+        "residual_field_count": len(residuals),
+        "residual_record_count": sum(len(values["initial"]) for values in residuals.values()),
+        "residuals": residual_summary,
+        "initial_residual_final_window_p95": max(
+            (record["initial_final_window_p95"] for record in residual_summary.values()
+             if record["initial_final_window_p95"] is not None),
+            default=None,
+        ),
+        "final_residual_final_window_p95": max(
+            (record["final_final_window_p95"] for record in residual_summary.values()
+             if record["final_final_window_p95"] is not None),
+            default=None,
+        ),
+        "courant_count": len(courants),
+        "courant_peak": max(courants) if courants else None,
+        "courant_final_window_p95": percentile(final_window(courants, contract), 0.95),
+        "continuity_count": len(continuity_global),
+        "continuity_global_final_window_p95": percentile(final_window(continuity_global, contract), 0.95),
+        "continuity_cumulative_final": continuity_cumulative[-1] if continuity_cumulative else None,
+    }
+
+
+def threshold(reference: float, key: str, contract: dict[str, Any] = DEFAULT_CONTRACT) -> float:
+    policy = contract[key]
+    return max(abs(reference) * float(policy["reference_factor"]), float(policy["absolute_floor"]))
+
+
+def compatible(
+    candidate: float | None,
+    reference: float | None,
+    key: str,
+    contract: dict[str, Any] = DEFAULT_CONTRACT,
+) -> tuple[bool | None, float | None]:
+    if reference is None:
+        return None, None
+    limit = threshold(reference, key, contract)
+    return candidate is not None and math.isfinite(candidate) and candidate <= limit, limit
+
+
+def _field_health(candidate: dict[str, Any], case_dir: Path | None) -> tuple[bool | None, bool | None, dict[str, Any]]:
+    health = candidate.get("health")
+    if not isinstance(health, dict):
+        health = final_field_health(case_dir)
+        checks = health.get("checks", {})
+        return checks.get("parsed_fields_finite"), checks.get("applicable_field_bounds_valid"), health
+    checks = health.get("checks") if isinstance(health.get("checks"), dict) else {}
+    finite = checks.get("all_parsed_fields_finite")
+    bounds = checks.get("applicable_field_bounds_valid")
+    if not isinstance(finite, bool) or not isinstance(bounds, bool):
+        fallback = final_field_health(case_dir)
+        fallback_checks = fallback.get("checks", {})
+        finite = finite if isinstance(finite, bool) else fallback_checks.get("parsed_fields_finite")
+        bounds = bounds if isinstance(bounds, bool) else fallback_checks.get("applicable_field_bounds_valid")
+        health = {"candidate_health": health, "independent_field_health": fallback}
+    return finite if isinstance(finite, bool) else None, bounds if isinstance(bounds, bool) else None, health
+
+
+def evaluate_numerical(
+    artifact: CaseArtifact,
+    *,
+    execution_pass: bool,
+    qoi_candidate: dict[str, Any],
+    reference_logs: list[Path] | tuple[Path, ...] = (),
+    reference_case_dir: Path | None = None,
+    reference_qois: dict[str, Any] | None = None,
+    reference_statistics: dict[str, Any] | None = None,
+    steady_plateau_enabled: bool = False,
+    check_mesh: bool = False,
+    mesh_timeout: float = 120.0,
+    contract: dict[str, Any] = DEFAULT_CONTRACT,
+) -> dict[str, Any]:
+    if not execution_pass:
+        return {
+            "schema_version": "foambench.numerical_validity.v2",
+            "status": "not_evaluated_execution_failure",
+            "pass": False,
+            "checks": {},
+            "failed_checks": [],
+        }
+    candidate = parse_logs(artifact.solver_logs, contract)
+    reference = (dict(reference_statistics) if reference_statistics is not None
+                 else parse_logs(reference_logs, contract) if reference_logs else {})
+    finite_fields, bounded_fields, health = _field_health(qoi_candidate, artifact.case_dir)
+    mesh = mesh_evidence(artifact.solver_logs)
+    if check_mesh and mesh["status"] == "unavailable":
+        mesh = run_check_mesh(artifact.case_dir, mesh_timeout)
+    latest, latest_dirs, layout = final_time_dirs(artifact.case_dir)
+    scheme = numerical_scheme(artifact.case_dir) if artifact.case_dir else "unknown"
+    plateau: dict[str, Any] = {"status": "not_applicable", "applicable": False}
+    reference_plateau: dict[str, Any] = {"status": "not_applicable", "applicable": False}
+    if steady_plateau_enabled and scheme == "steadyState" and reference_qois:
+        reference_plateau = steady_plateau(reference_qois)
+        baseline = {
+            name: float(metric["relative_span"])
+            for name, metric in reference_plateau.get("metrics", {}).items()
+            if isinstance(metric, dict) and isinstance(metric.get("relative_span"), (int, float))
+        }
+        plateau = steady_plateau(qoi_candidate.get("qois", {}), baseline)
+
+    relative = {
+        "final_linear_residual_reference_compatible": compatible(
+            candidate["final_residual_final_window_p95"], reference.get("final_residual_final_window_p95"),
+            "final_linear_residual", contract,
+        ),
+        "initial_residual_reference_compatible": compatible(
+            candidate["initial_residual_final_window_p95"], reference.get("initial_residual_final_window_p95"),
+            "initial_residual", contract,
+        ),
+        "courant_final_reference_compatible": compatible(
+            candidate["courant_final_window_p95"], reference.get("courant_final_window_p95"),
+            "courant_final_p95", contract,
+        ),
+        "courant_peak_reference_compatible": compatible(
+            candidate["courant_peak"], reference.get("courant_peak"), "courant_peak", contract,
+        ),
+        "continuity_reference_compatible": compatible(
+            candidate["continuity_global_final_window_p95"], reference.get("continuity_global_final_window_p95"),
+            "continuity_global_p95", contract,
+        ),
+        "continuity_cumulative_reference_compatible": compatible(
+            candidate["continuity_cumulative_final"], reference.get("continuity_cumulative_final"),
+            "continuity_cumulative_final", contract,
+        ),
+    }
+    checks: dict[str, dict[str, Any]] = {
+        "solver_log_present": {"status": "pass" if candidate["log_paths"] else "fail", "required": True},
+        "no_fatal_marker": {"status": "fail" if candidate["fatal_marker"] else "pass", "required": True},
+        "no_nonfinite_log_marker": {"status": "fail" if candidate["nonfinite_marker"] else "pass", "required": True},
+        "residual_evidence_present": {
+            "status": "pass" if candidate["residual_record_count"] else "fail",
+            "required": True,
+        },
+        "final_fields_present": {"status": "pass" if latest_dirs else "fail", "required": True},
+        "mesh_core_valid": {
+            "status": mesh["status"],
+            "required": mesh["status"] != "unavailable",
+        },
+        "steady_principal_qoi_plateau": {
+            "status": plateau["status"],
+            "required": bool(plateau.get("applicable")),
+        },
+        "all_parsed_final_fields_finite": {
+            "status": "not_applicable" if finite_fields is None else "pass" if finite_fields else "fail",
+            "required": finite_fields is not None,
+        },
+        "applicable_field_bounds_valid": {
+            "status": "not_applicable" if bounded_fields is None else "pass" if bounded_fields else "fail",
+            "required": bounded_fields is not None,
+        },
+    }
+    for name, (passed, limit) in relative.items():
+        checks[name] = {
+            "status": "not_applicable" if passed is None else "pass" if passed else "fail",
+            "required": passed is not None,
+            "limit": limit,
+        }
+    failed = [name for name, value in checks.items() if value["required"] and value["status"] == "fail"]
+    return {
+        "schema_version": "foambench.numerical_validity.v2",
+        "status": "pass" if not failed else "fail",
+        "pass": not failed,
+        "checks": checks,
+        "failed_checks": failed,
+        "candidate_logs": candidate,
+        "reference_logs": reference or None,
+        "candidate_latest_time": latest,
+        "final_field_layout": layout,
+        "field_health": health,
+        "mesh": mesh,
+        "time_scheme": scheme,
+        "steady_plateau": plateau,
+        "reference_steady_plateau": reference_plateau,
+    }
diff --git a/benchmarks/evaluation/pipeline.py b/benchmarks/evaluation/pipeline.py
new file mode 100644
index 0000000000000000000000000000000000000000..e16b2937dc4bea4c5b68d4135162cdafb6f7404b
--- /dev/null
+++ b/benchmarks/evaluation/pipeline.py
@@ -0,0 +1,166 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from .adapters import create_adapter
+from .aggregate import aggregate_results
+from .execution import evaluate_execution
+from .io import utc_now, write_json
+from .models import BenchmarkProfile, CaseArtifact
+from .numerical import evaluate_numerical
+from .profiles import expected_completion_time, load_assets
+from .qoi import evaluate_qoi
+from .reference import reference_case_dir, reference_log_paths, reference_statistics
+from .reporting import write_case_csv, write_summary_csv
+from .schema import validate
+
+
+def missing_artifact(case_id: str, profile: BenchmarkProfile, run_root: Path) -> CaseArtifact:
+    family, variant = profile.identity(case_id)
+    return CaseArtifact(
+        case_id=case_id,
+        dataset=profile.dataset,
+        family=family,
+        variant=variant,
+        replicate=1,
+        rollout_dir=run_root / family / variant / "replicate_001",
+        case_dir=None,
+        manifest={"status": "missing_rollout"},
+    )
+
+
+def failure_categories(result: dict[str, Any]) -> list[str]:
+    categories = []
+    if not result["scores"]["execution_pass"]:
+        categories.append("execution_failure")
+    elif not result["scores"]["numerical_pass"]:
+        categories.append("numerical_failure")
+    if result["scores"]["execution_pass"] and not result["scores"]["physics_grounded_qoi_pass"]:
+        qoi_status = result["qoi"].get("status")
+        if qoi_status == "evaluation_error":
+            categories.append("qoi_evaluation_error")
+        else:
+            categories.append("qoi_incomplete" if "incomplete" in str(qoi_status) else "qoi_out_of_tolerance")
+    return categories
+
+
+def evaluate_case(
+    artifact: CaseArtifact,
+    profile: BenchmarkProfile,
+    benchmark_case: dict[str, Any],
+    reference: dict[str, Any],
+    *,
+    check_mesh: bool = False,
+    mesh_timeout: float = 120.0,
+) -> dict[str, Any]:
+    execution = evaluate_execution(artifact, expected_completion_time(benchmark_case, reference))
+    execution_pass = execution["status"] == "pass"
+    qoi = evaluate_qoi(artifact, profile, reference, execution_pass=execution_pass)
+    numerical = evaluate_numerical(
+        artifact,
+        execution_pass=execution_pass,
+        qoi_candidate=qoi["candidate"],
+        reference_logs=reference_log_paths(profile, artifact.case_id),
+        reference_statistics=reference_statistics(profile, artifact.case_id),
+        reference_case_dir=reference_case_dir(profile, artifact.case_id),
+        # Numerical plateau is a stability check over available histories. It is
+        # deliberately separate from the principal Physics-grounded QoI roles.
+        reference_qois=dict(reference.get("qois", {})),
+        steady_plateau_enabled=bool(profile.numerical_contract.get("steady_qoi_plateau")),
+        check_mesh=check_mesh,
+        mesh_timeout=mesh_timeout,
+    )
+    numerical_pass = bool(numerical.get("pass"))
+    physics_grounded_qoi_pass = bool(qoi.get("physics_grounded_qoi_pass"))
+    result = {
+        "schema_version": "foambench.case_evaluation.v1",
+        "case_id": artifact.case_id,
+        "dataset": artifact.dataset,
+        "family": artifact.family,
+        "variant": artifact.variant,
+        "replicate": artifact.replicate,
+        "execution": execution,
+        "numerical": numerical,
+        "qoi": qoi,
+        "scores": {
+            "execution_pass": execution_pass,
+            "numerical_pass": numerical_pass,
+            "physics_grounded_qoi_pass": physics_grounded_qoi_pass,
+            "end_to_end_pass": execution_pass and numerical_pass and physics_grounded_qoi_pass,
+        },
+        "resources": {
+            "duration_seconds": artifact.duration_seconds,
+            "token_usage": artifact.token_usage,
+        },
+        "artifact": {
+            "rollout_dir": str(artifact.rollout_dir),
+            "workspace_dir": str(artifact.workspace_dir) if artifact.workspace_dir else None,
+            "case_dir": str(artifact.case_dir) if artifact.case_dir else None,
+        },
+    }
+    result["failure_categories"] = failure_categories(result)
+    return result
+
+
+def evaluate_campaign(
+    profile: BenchmarkProfile,
+    *,
+    adapter_name: str,
+    run_root: Path,
+    output_dir: Path | None = None,
+    check_mesh: bool = False,
+    mesh_timeout: float = 120.0,
+) -> dict[str, Any]:
+    benchmark, references = load_assets(profile)
+    adapter = create_adapter(adapter_name, run_root, profile)
+    discovered = adapter.discover()
+    unknown = sorted(set(discovered) - set(references))
+    if unknown:
+        raise ValueError("run contains cases outside the benchmark profile: " + ", ".join(unknown))
+    results = []
+    for case_id in sorted(references):
+        artifact = discovered.get(case_id) or missing_artifact(case_id, profile, run_root)
+        results.append(evaluate_case(
+            artifact, profile, benchmark[case_id], references[case_id],
+            check_mesh=check_mesh, mesh_timeout=mesh_timeout,
+        ))
+    overall = aggregate_results(results)
+    families = {
+        family: aggregate_results([row for row in results if row["family"] == family])
+        for family in sorted({row["family"] for row in results})
+    }
+    report = {
+        "schema_version": "foambench.campaign_evaluation.v1",
+        "generated_at": utc_now(),
+        "profile_id": profile.profile_id,
+        "dataset": profile.dataset,
+        "adapter": adapter_name,
+        "run_root": str(run_root.resolve()),
+        "reference_qois": str(profile.reference_qois_path),
+        "definitions": {
+            "execution_pass": "independent execution contract passed",
+            "numerical_pass": "execution passed and independent numerical contract passed",
+            "physics_grounded_qoi_pass": "execution passed and every principal Physics-grounded QoI passed its physical contract",
+            "end_to_end_pass": "execution_pass AND numerical_pass AND physics_grounded_qoi_pass",
+        },
+        "overall": overall,
+        "families": families,
+        "cases": {row["case_id"]: row for row in results},
+    }
+    validate(report, "benchmark_evaluation.schema.json")
+    if output_dir is not None:
+        output_dir = output_dir.resolve()
+        write_json(output_dir / "campaign_evaluation.json", report)
+        write_json(output_dir / "summary.json", {
+            key: report[key] for key in (
+                "schema_version", "generated_at", "profile_id", "dataset", "adapter",
+                "run_root", "definitions", "overall", "families",
+            )
+        })
+        case_root = output_dir / "cases"
+        for row in results:
+            write_json(case_root / row["family"] / f"{row['variant']}.json", row)
+        write_case_csv(output_dir / "cases.csv", results)
+        write_summary_csv(output_dir / "summary.csv", overall, families)
+    return report
diff --git a/benchmarks/evaluation/preparation.py b/benchmarks/evaluation/preparation.py
new file mode 100644
index 0000000000000000000000000000000000000000..cc4763925d3a13e9aad1c5cbfc7e7bcf1b46eca2
--- /dev/null
+++ b/benchmarks/evaluation/preparation.py
@@ -0,0 +1,172 @@
+from __future__ import annotations
+
+import re
+import subprocess
+from concurrent.futures import ThreadPoolExecutor, as_completed
+from pathlib import Path
+from typing import Any
+
+from .foam import read_text
+from .adapters import create_adapter
+from .execution import evaluate_execution
+from .io import write_json
+from .models import BenchmarkProfile, CaseArtifact
+from .profiles import expected_completion_time, load_assets
+
+
+WRITE_FORMAT_RE = re.compile(r"(?m)^\s*writeFormat\s+(ascii|binary)\s*;")
+
+
+def _patch_names(case_dir: Path) -> set[str]:
+    boundary = case_dir / "constant" / "polyMesh" / "boundary"
+    if not boundary.is_file():
+        return set()
+    text = boundary.read_text(encoding="utf-8", errors="ignore")
+    return set(re.findall(r"(?m)^\s*([A-Za-z_][A-Za-z0-9_]*)\s*\n\s*\{", text))
+
+
+def _run(command: list[str], log: Any, timeout: int) -> dict[str, Any]:
+    try:
+        completed = subprocess.run(
+            command,
+            stdout=log,
+            stderr=subprocess.STDOUT,
+            check=False,
+            text=True,
+            timeout=timeout,
+        )
+        return {"command": command, "return_code": completed.returncode, "timed_out": False}
+    except subprocess.TimeoutExpired:
+        return {"command": command, "return_code": None, "timed_out": True}
+    except OSError as exc:
+        return {"command": command, "return_code": 127, "timed_out": False, "error": str(exc)}
+
+
+def prepare_case(artifact: CaseArtifact, output_root: Path) -> dict[str, Any]:
+    case_dir = artifact.case_dir
+    if case_dir is None:
+        return {"case_id": artifact.case_id, "status": "skipped", "reason": "case_directory_missing"}
+    case_output = output_root / artifact.family / artifact.variant
+    case_output.mkdir(parents=True, exist_ok=True)
+    log_path = case_output / "preparation.log"
+    records: list[dict[str, Any]] = []
+    control_path = case_dir / "system" / "controlDict"
+    original_format_match = WRITE_FORMAT_RE.search(read_text(control_path))
+    original_format = original_format_match.group(1) if original_format_match else None
+    functions = ["writeCellCentres", "writeCellVolumes", "vorticity"]
+    # Sampling is measurement-only and deterministic when the candidate has
+    # explicitly declared the benchmark's system/sample dictionary.  Do not
+    # invent sample coordinates for cases that did not provide this contract.
+    if (case_dir / "system" / "sample").is_file():
+        functions.append("sample")
+    patches = _patch_names(case_dir)
+    if artifact.family == "supersonicCrossJet":
+        # Patch names vary between the fixed reference (inlet1/inlet2) and
+        # agent cases (inlet/jet).  Resolve only semantically named patches.
+        selected = sorted(name for name in patches if any(token in name.lower() for token in ("inlet", "jet")))
+        functions.extend(f"patchFlowRate(phi,patch={name})" for name in selected)
+    elif artifact.family in {"ERCOFTA_pump", "nozzleCDV"}:
+        selected = sorted(name for name in patches if any(token in name.lower() for token in ("inlet", "outlet")))
+        functions.extend(f"patchFlowRate(phi,patch={name})" for name in selected)
+        functions.extend(f"patchAverage(p,patch={name})" for name in selected)
+    with log_path.open("w", encoding="utf-8") as log:
+        for function_name in functions:
+            command = ["foamPostProcess", "-case", str(case_dir), "-func", function_name]
+            # Preparation is intentionally endpoint-only.  A single retained
+            # endpoint cannot support a transient-history claim, so histories
+            # remain diagnostic unless the candidate already saved them.
+            command.append("-latestTime")
+            record = _run(command, log, 300)
+            record["required"] = function_name != "sample"
+            records.append(record)
+        if original_format == "binary":
+            set_ascii = [
+                "foamDictionary", "-case", str(case_dir), "system/controlDict",
+                "-entry", "writeFormat", "-set", "ascii",
+            ]
+            restore = [
+                "foamDictionary", "-case", str(case_dir), "system/controlDict",
+                "-entry", "writeFormat", "-set", "binary",
+            ]
+            record = _run(set_ascii, log, 60)
+            record["required"] = True
+            records.append(record)
+            try:
+                record = _run([
+                    "foamFormatConvert", "-case", str(case_dir), "-latestTime",
+                ], log, 300)
+                record["required"] = True
+                records.append(record)
+            finally:
+                record = _run(restore, log, 60)
+                record["required"] = True
+                records.append(record)
+    failed = [
+        record for record in records
+        if record.get("required", True) and record.get("return_code") != 0
+    ]
+    optional_failures = [
+        record for record in records
+        if not record.get("required", True) and record.get("return_code") != 0
+    ]
+    result = {
+        "case_id": artifact.case_id,
+        "case_dir": str(case_dir),
+        "status": "pass" if not failed else "fail",
+        "role": "measurement_only",
+        "original_write_format": original_format,
+        "log": str(log_path),
+        "commands": records,
+        "optional_failures": optional_failures,
+    }
+    write_json(case_output / "preparation.json", result)
+    return result
+
+
+def prepare_cases(artifacts: list[CaseArtifact], output_root: Path, jobs: int) -> dict[str, Any]:
+    output_root.mkdir(parents=True, exist_ok=True)
+    records = []
+    with ThreadPoolExecutor(max_workers=max(1, jobs)) as executor:
+        futures = {executor.submit(prepare_case, artifact, output_root): artifact for artifact in artifacts}
+        for future in as_completed(futures):
+            artifact = futures[future]
+            try:
+                records.append(future.result())
+            except Exception as exc:
+                records.append({"case_id": artifact.case_id, "status": "error", "error": str(exc)})
+    records.sort(key=lambda record: record["case_id"])
+    report = {
+        "role": "measurement_only",
+        "case_count": len(records),
+        "pass_count": sum(record["status"] == "pass" for record in records),
+        "fail_count": sum(record["status"] != "pass" for record in records),
+        "cases": records,
+    }
+    write_json(output_root / "preparation_summary.json", report)
+    return report
+
+
+def prepare_campaign(
+    profile: BenchmarkProfile,
+    *,
+    adapter_name: str,
+    run_root: Path,
+    output_root: Path,
+    jobs: int = 1,
+) -> dict[str, Any]:
+    """Prepare derived field QoIs for execution-complete field campaigns."""
+    if profile.extractor not in {"field", "extended"}:
+        raise ValueError("preparation is only applicable to field and Extended QoI profiles")
+    benchmark, references = load_assets(profile)
+    artifacts = create_adapter(adapter_name, run_root, profile).discover()
+    eligible = []
+    for case_id, artifact in artifacts.items():
+        reference = references.get(case_id)
+        if reference is None:
+            continue
+        execution = evaluate_execution(
+            artifact, expected_completion_time(benchmark[case_id], reference)
+        )
+        if execution["status"] == "pass":
+            eligible.append(artifact)
+    return prepare_cases(eligible, output_root, jobs)
diff --git a/benchmarks/evaluation/profiles.py b/benchmarks/evaluation/profiles.py
new file mode 100644
index 0000000000000000000000000000000000000000..2a5aa19e172fe32ab8191e1f6b549d5f3b0c65f7
--- /dev/null
+++ b/benchmarks/evaluation/profiles.py
@@ -0,0 +1,74 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from .io import read_object
+from .models import BenchmarkProfile
+from .schema import validate
+
+
+def load_assets(profile: BenchmarkProfile) -> tuple[dict[str, Any], dict[str, Any]]:
+    benchmark = read_object(profile.benchmark_path)
+    reference_document = read_object(profile.reference_qois_path)
+    validate(reference_document, "foambench_qoi_reference.schema.json")
+    references = reference_document.get("cases")
+    if not isinstance(references, dict):
+        raise ValueError(f"reference QoI file has no cases object: {profile.reference_qois_path}")
+    if len(references) != profile.expected_case_count:
+        raise ValueError(
+            f"profile membership mismatch: expected {profile.expected_case_count}, got {len(references)}"
+        )
+    current_design = (
+        read_object(profile.benchmark_path.parent / "FoamBench_extended_openfoam13_qoi_design.json")
+        if profile.extractor == "extended" else None
+    )
+    for case_id, reference in references.items():
+        principal = reference.get("principal_metrics", [])
+        qois = reference.get("qois", {})
+        tolerances = reference.get("tolerances", {})
+        missing_values = sorted(set(principal) - set(qois))
+        missing_tolerances = sorted(set(principal) - set(tolerances))
+        if missing_values or missing_tolerances:
+            raise ValueError(
+                f"reference QoI contract incomplete for {case_id}: "
+                f"missing_values={missing_values}, missing_tolerances={missing_tolerances}"
+            )
+        if profile.extractor == "extended":
+            from .extbench import design_case_contract
+
+            expected_branch, expected_principal = design_case_contract(case_id, current_design or {})
+            if reference.get("branch_id") != expected_branch:
+                raise ValueError(
+                    f"ExtBench branch drift for {case_id}: "
+                    f"reference={reference.get('branch_id')!r}, design={expected_branch!r}"
+                )
+            if set(principal) != set(expected_principal):
+                raise ValueError(
+                    f"ExtBench principal-metric drift for {case_id}: "
+                    f"reference={sorted(principal)}, design={sorted(expected_principal)}"
+                )
+    benchmark_cases = benchmark.get("cases") if isinstance(benchmark.get("cases"), dict) else benchmark
+    if not isinstance(benchmark_cases, dict):
+        raise ValueError(f"benchmark has no case mapping: {profile.benchmark_path}")
+    missing = sorted(set(references) - set(benchmark_cases))
+    if missing:
+        raise ValueError("benchmark is missing reference cases: " + ", ".join(missing))
+    return benchmark_cases, references
+
+
+def expected_end_time(case: dict[str, Any]) -> float | None:
+    text = case.get("system/controlDict")
+    if not isinstance(text, str):
+        return None
+    import re
+
+    match = re.search(r"(?m)^\s*endTime\s+([-+0-9.eE]+)\s*;", text)
+    return float(match.group(1)) if match else None
+
+
+def expected_completion_time(case: dict[str, Any], reference: dict[str, Any]) -> float | None:
+    latest = reference.get("latest_time")
+    if isinstance(latest, (int, float)):
+        return float(latest)
+    return expected_end_time(case)
diff --git a/benchmarks/evaluation/profiles/advanced.json b/benchmarks/evaluation/profiles/advanced.json
new file mode 100644
index 0000000000000000000000000000000000000000..d1c0bf76660739dd16fd08bdd302489d3f8f6eb5
--- /dev/null
+++ b/benchmarks/evaluation/profiles/advanced.json
@@ -0,0 +1,19 @@
+{
+  "profile_id": "foambench.advanced.v1",
+  "dataset": "advanced",
+  "benchmark_path": "benchmarks/FoamBench_advanced_openfoam13_fixed_final.json",
+  "reference_qois_path": "benchmarks/FoamBench_advanced_openfoam13_reference_qois.json",
+  "membership": {
+    "expected_case_count": 16,
+    "case_id_style": "case_name"
+  },
+  "qoi": {
+    "extractor": "field",
+    "required_fraction": 1.0
+  },
+  "numerical": {
+    "contract": "physics_grounded_qoi.v1",
+    "steady_qoi_plateau": true,
+    "reference_statistics_path": "benchmarks/reference_statistics/advanced.json"
+  }
+}
diff --git a/benchmarks/evaluation/profiles/basic.json b/benchmarks/evaluation/profiles/basic.json
new file mode 100644
index 0000000000000000000000000000000000000000..7e1915a057e14896decbf7cc87d81fbfe7915c04
--- /dev/null
+++ b/benchmarks/evaluation/profiles/basic.json
@@ -0,0 +1,19 @@
+{
+  "profile_id": "foambench.basic.v1",
+  "dataset": "basic",
+  "benchmark_path": "benchmarks/FoamBench_basic_openfoam13_fixed_final.json",
+  "reference_qois_path": "benchmarks/FoamBench_basic_openfoam13_reference_qois.json",
+  "membership": {
+    "expected_case_count": 110,
+    "case_id_style": "family_variant"
+  },
+  "qoi": {
+    "extractor": "field",
+    "required_fraction": 1.0
+  },
+  "numerical": {
+    "contract": "physics_grounded_qoi.v1",
+    "steady_qoi_plateau": true,
+    "reference_statistics_path": "benchmarks/reference_statistics/basic.json"
+  }
+}
diff --git a/benchmarks/evaluation/profiles/extended.json b/benchmarks/evaluation/profiles/extended.json
new file mode 100644
index 0000000000000000000000000000000000000000..42957f6a72678559870890415fbb1585f4096951
--- /dev/null
+++ b/benchmarks/evaluation/profiles/extended.json
@@ -0,0 +1,19 @@
+{
+  "profile_id": "foambench.extended",
+  "dataset": "extended",
+  "benchmark_path": "benchmarks/FoamBench_extended_openfoam13_fixed.json",
+  "reference_qois_path": "benchmarks/FoamBench_extended_openfoam13_reference_qois.json",
+  "membership": {
+    "expected_case_count": 100,
+    "case_id_style": "family_variant"
+  },
+  "qoi": {
+    "extractor": "extended",
+    "required_fraction": 1.0
+  },
+  "numerical": {
+    "contract": "foambench.qoi.design",
+    "tolerances": "joint_physical_admissibility_and_reference_response_provisional",
+    "reference_statistics_path": "benchmarks/reference_statistics/extended.json"
+  }
+}
diff --git a/benchmarks/evaluation/qoi.py b/benchmarks/evaluation/qoi.py
new file mode 100644
index 0000000000000000000000000000000000000000..0c3c0fa4562a3dd8d35bef9a9b6aabcb6e854a2b
--- /dev/null
+++ b/benchmarks/evaluation/qoi.py
@@ -0,0 +1,79 @@
+from __future__ import annotations
+
+from typing import Any
+
+from .comparison import compare_case
+from .extbench import extract_contract_case
+
+from .field_candidate import extract_field_candidate
+from .models import BenchmarkProfile, CaseArtifact
+from .schema import validate
+
+
+def empty_candidate(case_id: str, status: str, reason: str) -> dict[str, Any]:
+    return {
+        "schema_version": "foambench.qoi.candidate",
+        "case_id": case_id,
+        "status": status,
+        "qois": {},
+        "health": {"status": "not_assessed", "reason": reason},
+    }
+
+
+def evaluate_qoi(
+    artifact: CaseArtifact,
+    profile: BenchmarkProfile,
+    reference: dict[str, Any],
+    *,
+    execution_pass: bool,
+) -> dict[str, Any]:
+    if not execution_pass or artifact.case_dir is None:
+        return {
+            "status": "not_evaluated_execution_failure",
+            "physics_grounded_qoi_pass": False,
+            "effective_pass_ratio": 0.0,
+            "candidate": empty_candidate(
+                artifact.case_id, "not_evaluated_execution_failure", "execution_not_passed"
+            ),
+            "comparison": None,
+        }
+    try:
+        if profile.extractor == "extended":
+            candidate = extract_contract_case(artifact.case_dir, artifact.case_id)
+            required = candidate.get("required_metrics", [])
+        elif profile.extractor == "field":
+            required = reference.get("principal_metrics")
+            if not isinstance(required, list):
+                required = list(reference.get("qois", {}))
+            requested = list(reference.get("qois", {}))
+            candidate = extract_field_candidate(
+                artifact.case_dir,
+                artifact.case_id,
+                requested,
+                required_metrics=required,
+                log_paths=list(artifact.solver_logs),
+            )
+        else:
+            raise ValueError(f"unknown QoI extractor: {profile.extractor}")
+        validate(candidate, "foambench_qoi_candidate.schema.json")
+        comparison = compare_case(reference, candidate, profile.required_qoi_fraction)
+        validate(comparison, "foambench_qoi_comparison.schema.json")
+        health = candidate.get("health")
+        health_pass = not isinstance(health, dict) or health.get("status") in {None, "pass"}
+        physics_grounded_qoi = bool(comparison.get("physics_grounded_qoi_pass") and health_pass)
+        return {
+            "status": "pass" if physics_grounded_qoi else str(comparison.get("status", "fail")),
+            "physics_grounded_qoi_pass": physics_grounded_qoi,
+            "effective_pass_ratio": float(comparison.get("qoi_pass_ratio", 0.0)) if health_pass else 0.0,
+            "candidate": candidate,
+            "comparison": comparison,
+        }
+    except Exception as exc:
+        return {
+            "status": "evaluation_error",
+            "physics_grounded_qoi_pass": False,
+            "effective_pass_ratio": 0.0,
+            "candidate": empty_candidate(artifact.case_id, "error", str(exc)),
+            "comparison": None,
+            "error": str(exc),
+        }
diff --git a/benchmarks/evaluation/qoi_glue.py b/benchmarks/evaluation/qoi_glue.py
new file mode 100644
index 0000000000000000000000000000000000000000..0fafc4a6df8865e62a56221bdbf50e5fc031810d
--- /dev/null
+++ b/benchmarks/evaluation/qoi_glue.py
@@ -0,0 +1,493 @@
+#!/usr/bin/env python3
+"""Conservative LLM-assisted recovery for incomplete Extended QoI evidence.
+
+The model is an evidence router only.  It selects an existing file/column and
+an allow-listed deterministic operation; this module computes the observation
+and validates the source locally.  Reference QoI values are never included in
+the model packet.
+"""
+from __future__ import annotations
+
+import copy
+import csv
+import hashlib
+import json
+import math
+import os
+import re
+import subprocess
+from pathlib import Path
+from typing import Any
+
+
+ROOT = Path(__file__).resolve().parents[2]
+GLUE_VERSION = "foambench.qoi_glue.v1"
+PLAN_SCHEMA = ROOT / "schemas/qoi_recovery_plan.schema.json"
+TABLE_SUFFIXES = {".csv", ".dat", ".raw", ".xy"}
+TIME_COLUMN = "Time"
+MASS_COLUMNS = {
+    "rhophi",
+    "massflow",
+    "massflux",
+    "sumphi",
+    "areaintegratephi",
+}
+EXPECTED_BRANCHES = {"Re_tau_180", "Re_tau_395", "Re_tau_590"}
+
+
+def _enabled() -> bool:
+    return os.environ.get("EVOLUTION_QOI_GLUE", "off").strip().lower() in {
+        "1", "true", "on", "yes",
+    }
+
+
+def _model() -> str:
+    return (
+        os.environ.get("evolution_QOI_GLUE_MODEL")
+        or os.environ.get("evolution_EVALUATION_MODEL")
+        or "gpt-5.6-terra"
+    )
+
+
+def _reasoning() -> str | None:
+    return (
+        os.environ.get("evolution_QOI_GLUE_REASONING_EFFORT")
+        or os.environ.get("evolution_EVALUATION_REASONING_EFFORT")
+        or os.environ.get("evolution_REASONING_EFFORT")
+    )
+
+
+def _timeout() -> float:
+    raw = os.environ.get("EVOLUTION_QOI_GLUE_TIMEOUT", "180")
+    try:
+        return max(5.0, float(raw))
+    except ValueError:
+        return 180.0
+
+
+def _normalise(value: str) -> str:
+    return re.sub(r"[^a-z0-9]", "", value.lower().replace("+", "plus"))
+
+
+def _finite(value: Any) -> float | None:
+    if isinstance(value, bool) or not isinstance(value, (int, float)):
+        return None
+    result = float(value)
+    return result if math.isfinite(result) else None
+
+
+def _safe_source(case_dir: Path, raw: Any) -> Path:
+    if not isinstance(raw, str) or not raw or Path(raw).is_absolute():
+        raise ValueError("source must be a relative case path")
+    source = (case_dir / raw).resolve(strict=True)
+    if not source.is_relative_to(case_dir.resolve(strict=True)):
+        raise ValueError("source escapes the case directory")
+    if not source.is_file():
+        raise ValueError("source is not a file")
+    return source
+
+
+def _evidence_path(case_dir: Path, source: Path) -> str:
+    return source.relative_to(case_dir.resolve(strict=True)).as_posix()
+
+
+def _field_dimensions(case_dir: Path, field: str) -> str | None:
+    for path in sorted(case_dir.rglob(field), reverse=True):
+        if not path.is_file() or not path.parent.name.replace(".", "", 1).isdigit():
+            continue
+        text = path.read_bytes()[:4096].decode("ascii", errors="ignore")
+        match = re.search(r"dimensions\s*\[([^]]+)\]", text)
+        if match:
+            return " ".join(match.group(1).split())
+    return None
+
+
+def _named_numeric_rows(path: Path) -> tuple[list[str], list[list[float]]]:
+    """Read a compatible numeric table without accepting arbitrary prose."""
+    headers: list[list[str]] = []
+    rows: list[list[float]] = []
+    for line in path.read_text(encoding="utf-8", errors="ignore").splitlines():
+        stripped = line.strip()
+        if not stripped:
+            continue
+        if stripped.startswith("#"):
+            names = stripped[1:].strip().replace(",", " ").replace("\t", " ").split()
+            if names:
+                headers.append(names)
+            continue
+        parts = stripped.replace("(", " ").replace(")", " ").replace(",", " ").split()
+        if parts and all(re.fullmatch(r"[-+0-9.eE]+", item) for item in parts):
+            rows.append([float(item) for item in parts])
+        elif not rows and ("," in stripped or "\t" in stripped):
+            names = [item.strip() for item in stripped.split(",")] if "," in stripped else stripped.split("\t")
+            if names:
+                headers.append(names)
+    if not rows:
+        return [], []
+    width = len(rows[0])
+    header = next((names for names in reversed(headers) if len(names) == width), [])
+    return header, [row for row in rows if len(row) == width]
+
+
+def _case_fingerprint(case_dir: Path) -> str:
+    digest = hashlib.sha256()
+    for path in sorted(item for item in case_dir.rglob("*") if item.is_file()):
+        relative = path.relative_to(case_dir).as_posix().encode("utf-8")
+        digest.update(len(relative).to_bytes(8, "big"))
+        digest.update(relative)
+        digest.update(path.stat().st_size.to_bytes(8, "big"))
+        with path.open("rb") as stream:
+            for block in iter(lambda: stream.read(1024 * 1024), b""):
+                digest.update(block)
+    return digest.hexdigest()
+
+
+def _inventory(case_dir: Path) -> list[dict[str, Any]]:
+    entries: list[dict[str, Any]] = []
+    candidates = [item for item in case_dir.rglob("*") if item.is_file()]
+    candidates.sort(key=lambda item: (item.suffix.lower() not in TABLE_SUFFIXES, str(item)))
+    for path in candidates[:180]:
+        relative = path.relative_to(case_dir).as_posix()
+        item: dict[str, Any] = {"path": relative, "bytes": path.stat().st_size}
+        if path.suffix.lower() in TABLE_SUFFIXES and path.stat().st_size <= 512 * 1024:
+            sample = path.read_text(encoding="utf-8", errors="ignore")[:1600]
+            item["sample"] = sample
+        elif path.name in {"phi", "C", "U", "Vc", "p", "alpha.water"}:
+            sample = path.read_bytes()[:4096].decode("ascii", errors="ignore")
+            match = re.search(r"dimensions\s*\[([^]]+)\]", sample)
+            if match:
+                item["dimensions"] = " ".join(match.group(1).split())
+        entries.append(item)
+    return entries
+
+
+def build_packet(
+    case_dir: Path,
+    case_id: str,
+    candidate: dict[str, Any],
+    comparison: dict[str, Any],
+) -> dict[str, Any]:
+    """Create the small, reference-free packet supplied to the model."""
+    return {
+        "schema_version": GLUE_VERSION,
+        "case_id": case_id,
+        "family": case_id.split("/", 1)[0] if "/" in case_id else case_id,
+        "required_metrics": list(candidate.get("required_metrics", [])),
+        "missing_metrics": list(candidate.get("missing_metrics", [])),
+        "extraction_errors": list(candidate.get("extraction_errors", [])),
+        "comparison_status": comparison.get("status"),
+        "allowed_operations": {
+            "table_time_history": "Read an explicit Time plus one flux column; preserve signed values and phi dimensions.",
+            "branch_spalding_table": "Split one labelled table by branch and compute branch wall-law scalars only when yPlus and spaldingYPlus columns exist.",
+        },
+        "files": _inventory(case_dir),
+    }
+
+
+def _prompt(packet: dict[str, Any]) -> str:
+    return (
+        "You are a conservative CFD measurement-evidence router.\n"
+        "Reference QoI values are unavailable and must not be requested or inferred.\n"
+        "Do not calculate or emit QoI numbers. Return only JSON matching the supplied schema.\n"
+        "Select an existing file and columns only when they are physically equivalent to a declared principal metric.\n"
+        "Use status=unrecoverable when evidence is absent, ambiguous, a proxy, or has the wrong physical quantity.\n"
+        "Allowed operations are exactly table_time_history and branch_spalding_table.\n\n"
+        "Evidence packet:\n" + json.dumps(packet, ensure_ascii=False, indent=2)
+    )
+
+
+def _cache_path(campaign_root: Path, case_dir: Path, case_id: str, missing: list[str], model: str) -> Path:
+    identity = {
+        "version": GLUE_VERSION,
+        "case_id": case_id,
+        "missing": sorted(missing),
+        "model": model,
+        "fingerprint": _case_fingerprint(case_dir),
+    }
+    key = hashlib.sha256(json.dumps(identity, sort_keys=True).encode("utf-8")).hexdigest()
+    return campaign_root / "cache" / "qoi_glue" / f"{key}.json"
+
+
+def _write_json(path: Path, value: Any) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    temporary.write_text(json.dumps(value, ensure_ascii=False, indent=2) + "\n", encoding="utf-8")
+    temporary.replace(path)
+
+
+def _load_cached(path: Path) -> dict[str, Any] | None:
+    if not path.is_file():
+        return None
+    try:
+        value = json.loads(path.read_text(encoding="utf-8"))
+    except (OSError, json.JSONDecodeError):
+        return None
+    return value if isinstance(value, dict) else None
+
+
+def _run_model(
+    case_dir: Path,
+    packet: dict[str, Any],
+    artifact: Path,
+) -> dict[str, Any]:
+    from scripts.evolution_adapter_common import codex_exec_command
+
+    model = _model()
+    artifact.parent.mkdir(parents=True, exist_ok=True)
+    final_message = artifact.with_suffix(".last_message.json")
+    trajectory = artifact.with_suffix(".trajectory.jsonl")
+    command = codex_exec_command(
+        case_dir,
+        final_message,
+        model,
+        output_schema=PLAN_SCHEMA if PLAN_SCHEMA.is_file() else None,
+        reasoning_effort=_reasoning(),
+        sandbox="read-only",
+    )
+    try:
+        completed = subprocess.run(
+            command,
+            input=_prompt(packet),
+            text=True,
+            encoding="utf-8",
+            errors="replace",
+            stdout=subprocess.PIPE,
+            stderr=subprocess.PIPE,
+            cwd=case_dir,
+            timeout=_timeout(),
+            check=False,
+        )
+    except (OSError, subprocess.TimeoutExpired) as exc:
+        return {
+            "status": "unavailable",
+            "model": model,
+            "error": str(exc),
+            "command": command,
+        }
+    trajectory.write_text(completed.stdout, encoding="utf-8")
+    if completed.returncode != 0:
+        return {
+            "status": "unavailable",
+            "model": model,
+            "return_code": completed.returncode,
+            "stderr_tail": completed.stderr[-2000:],
+            "command": command,
+        }
+    try:
+        plan = json.loads(final_message.read_text(encoding="utf-8"))
+    except (OSError, json.JSONDecodeError) as exc:
+        return {
+            "status": "invalid_response",
+            "model": model,
+            "error": str(exc),
+            "stderr_tail": completed.stderr[-2000:],
+        }
+    if not isinstance(plan, dict):
+        return {"status": "invalid_response", "model": model, "error": "plan is not an object"}
+    return {
+        "status": "received",
+        "model": model,
+        "return_code": completed.returncode,
+        "plan": plan,
+        "stderr_tail": completed.stderr[-2000:],
+    }
+
+
+def _validate_mapping(mapping: dict[str, Any], required: set[str]) -> None:
+    metric = mapping.get("metric")
+    if not isinstance(metric, str) or metric not in required:
+        raise ValueError("mapping metric is not a missing principal metric")
+    operation = mapping.get("operation")
+    if operation not in {"table_time_history", "branch_spalding_table"}:
+        raise ValueError("operation is not allow-listed")
+    if operation == "table_time_history":
+        column = mapping.get("column")
+        if not isinstance(column, str) or not column:
+            raise ValueError("table_time_history requires a column")
+    if operation == "branch_spalding_table":
+        if metric != "branchwise_wall_law_metrics":
+            raise ValueError("branch_spalding_table has one supported metric")
+        if mapping.get("branch_column") != "branch":
+            raise ValueError("branch_spalding_table requires a branch column")
+
+
+def _execute_time_history(case_dir: Path, mapping: dict[str, Any]) -> tuple[dict[str, Any], list[str]]:
+    source = _safe_source(case_dir, mapping.get("source"))
+    header, rows = _named_numeric_rows(source)
+    if TIME_COLUMN not in header:
+        raise ValueError("table has no Time column")
+    column = str(mapping["column"])
+    if column not in header or _normalise(column) not in MASS_COLUMNS:
+        raise ValueError("column is not an allow-listed explicit flux column")
+    if "inlet" not in str(source).lower() and str(mapping.get("patch", "")).lower() not in {"inlet", "inlet1", "main"}:
+        raise ValueError("mass-flow source is not identified as an inlet")
+    dimensions = _field_dimensions(case_dir, "phi")
+    quantity = {
+        "1 0 -1 0 0 0 0": "explicit_mass_flow",
+        "0 3 -1 0 0 0 0": "explicit_volumetric_flow",
+    }.get(dimensions)
+    if quantity is None:
+        raise ValueError("phi dimensions are absent or unsupported")
+    time_index, value_index = header.index(TIME_COLUMN), header.index(column)
+    points = [
+        {"time": row[time_index], "value": row[value_index]}
+        for row in rows
+        if math.isfinite(row[time_index]) and math.isfinite(row[value_index])
+    ]
+    if not points:
+        raise ValueError("table has no finite history points")
+    branch = "root"
+    parent = source.relative_to(case_dir).parts
+    if "postProcessing" in parent:
+        branch = "/".join(parent[: parent.index("postProcessing")]) or "root"
+    history: dict[str, Any] = {
+        "kind": "time_history",
+        "quantity": quantity,
+        "field_dimensions": dimensions,
+        "points": sorted(points, key=lambda item: item["time"]),
+    }
+    if branch != "root":
+        history = {
+            "kind": "branched_time_histories",
+            "quantity": quantity,
+            "field_dimensions": dimensions,
+            "branches": {branch: history},
+        }
+    return history, [_evidence_path(case_dir, source)]
+
+
+def _csv_rows(path: Path) -> tuple[list[str], list[dict[str, str]]]:
+    with path.open(newline="", encoding="utf-8", errors="ignore") as stream:
+        reader = csv.DictReader(stream)
+        rows = [dict(row) for row in reader if row]
+        return list(reader.fieldnames or []), rows
+
+
+def _execute_branch_spalding(case_dir: Path, mapping: dict[str, Any]) -> tuple[dict[str, Any], list[str]]:
+    source = _safe_source(case_dir, mapping.get("source"))
+    columns, rows = _csv_rows(source)
+    normalised = {_normalise(column): column for column in columns}
+    branch_name = normalised.get("branch")
+    y_name = normalised.get("yplus")
+    predicted_name = normalised.get("spaldingyplus")
+    if not branch_name or not y_name or not predicted_name:
+        raise ValueError("branch table requires branch, yPlus, and spaldingYPlus columns")
+    branches: dict[str, Any] = {}
+    for branch in EXPECTED_BRANCHES:
+        selected = [row for row in rows if row.get(branch_name) == branch]
+        if not selected:
+            raise ValueError(f"branch table is missing {branch}")
+        errors: list[float] = []
+        y_values: list[float] = []
+        for row in selected:
+            yplus = _finite(float(row[y_name])) if row.get(y_name) else None
+            predicted = _finite(float(row[predicted_name])) if row.get(predicted_name) else None
+            if yplus is None or predicted is None or yplus < 0 or predicted < 0:
+                continue
+            y_values.append(yplus)
+            errors.append(math.log1p(yplus) - math.log1p(predicted))
+        if not errors or not y_values:
+            raise ValueError(f"branch {branch} has no finite wall-law rows")
+        branches[branch] = {
+            "first_cell_yplus": min(y_values),
+            "spalding_log_rmse": math.sqrt(sum(item * item for item in errors) / len(errors)),
+        }
+    return {"kind": "branch_scalars", "branches": branches}, [_evidence_path(case_dir, source)]
+
+
+def apply_plan(
+    case_dir: Path,
+    candidate: dict[str, Any],
+    plan: dict[str, Any],
+) -> tuple[dict[str, Any], dict[str, Any]]:
+    """Apply a validated plan; any ambiguity leaves the candidate unchanged."""
+    if plan.get("status") != "recoverable":
+        return copy.deepcopy(candidate), {"status": str(plan.get("status", "unrecoverable")), "reason": plan.get("reason")}
+    mappings = plan.get("mappings")
+    required = set(candidate.get("missing_metrics", []))
+    if not isinstance(mappings, list) or not mappings:
+        return copy.deepcopy(candidate), {"status": "invalid_plan", "reason": "recoverable plan has no mappings"}
+    result = copy.deepcopy(candidate)
+    selected: dict[str, Any] = {}
+    try:
+        for mapping in mappings:
+            if not isinstance(mapping, dict):
+                raise ValueError("mapping is not an object")
+            _validate_mapping(mapping, required)
+            metric = str(mapping["metric"])
+            if metric in selected:
+                raise ValueError(f"duplicate mapping for {metric}")
+            if mapping["operation"] == "table_time_history":
+                value, evidence = _execute_time_history(case_dir, mapping)
+                method = "qoi_glue.table_time_history.v1"
+            else:
+                value, evidence = _execute_branch_spalding(case_dir, mapping)
+                method = "qoi_glue.branch_spalding_table.v1"
+            selected[metric] = {"value": value, "evidence": evidence, "method": method}
+    except (OSError, ValueError, TypeError, KeyError) as exc:
+        return copy.deepcopy(candidate), {"status": "rejected", "reason": str(exc), "plan": plan}
+    qois = result.setdefault("qois", {})
+    evidence = result.setdefault("evidence", {})
+    methods = result.setdefault("metric_methods", {})
+    resolver = result.setdefault("resolver_report", {})
+    for metric, item in selected.items():
+        qois[metric] = item["value"]
+        evidence[metric] = item["evidence"]
+        methods[metric] = item["method"]
+        resolver[metric] = {
+            "status": "selected",
+            "selected_evidence": item["evidence"],
+            "method": item["method"],
+            "physical_validation": "qoi_glue.allowlisted_operation.v1",
+        }
+    required_metrics = list(result.get("required_metrics", []))
+    missing = sorted(set(required_metrics) - set(qois))
+    result["missing_metrics"] = missing
+    extraction_errors = list(result.get("extraction_errors", []))
+    result["status"] = "complete" if not missing and not extraction_errors else "incomplete"
+    health = result.setdefault("health", {})
+    health["status"] = "pass" if not missing and not extraction_errors else "incomplete"
+    checks = health.setdefault("checks", {})
+    checks["principal_qoi_complete"] = not missing
+    checks["principal_extraction_error_free"] = not extraction_errors
+    return result, {
+        "status": "recovered_complete" if not missing and not extraction_errors else "recovered_partial",
+        "metrics": sorted(selected),
+        "evidence": {metric: item["evidence"] for metric, item in selected.items()},
+        "methods": {metric: item["method"] for metric, item in selected.items()},
+        "plan": plan,
+    }
+
+
+def recover_with_llm(
+    case_dir: Path,
+    case_id: str,
+    candidate: dict[str, Any],
+    comparison: dict[str, Any],
+    campaign_root: Path,
+) -> tuple[dict[str, Any], dict[str, Any]]:
+    """Recover one incomplete candidate, with one cached model call at most."""
+    if not _enabled():
+        return copy.deepcopy(candidate), {"status": "disabled", "version": GLUE_VERSION}
+    missing = list(candidate.get("missing_metrics", []))
+    if not missing:
+        return copy.deepcopy(candidate), {"status": "not_needed", "version": GLUE_VERSION}
+    model = _model()
+    artifact = _cache_path(campaign_root, case_dir, case_id, missing, model)
+    cached = _load_cached(artifact)
+    if cached is None:
+        packet = build_packet(case_dir, case_id, candidate, comparison)
+        cached = _run_model(case_dir, packet, artifact)
+        cached["version"] = GLUE_VERSION
+        cached["case_id"] = case_id
+        cached["missing_metrics"] = sorted(missing)
+        _write_json(artifact, cached)
+    plan = cached.get("plan") if isinstance(cached.get("plan"), dict) else {"status": cached.get("status", "unavailable")}
+    recovered, detail = apply_plan(case_dir, candidate, plan)
+    detail.update({
+        "version": GLUE_VERSION,
+        "artifact": str(artifact),
+        "model": cached.get("model", model),
+        "execution_status": cached.get("status"),
+    })
+    return recovered, detail
diff --git a/benchmarks/evaluation/qoi_reference.py b/benchmarks/evaluation/qoi_reference.py
new file mode 100644
index 0000000000000000000000000000000000000000..15f0f704343cc5dcba71bc8cf6d74a0930dad32e
--- /dev/null
+++ b/benchmarks/evaluation/qoi_reference.py
@@ -0,0 +1,566 @@
+#!/usr/bin/env python3
+"""Build canonical FoamBench QoI reference datasets from completed runs.
+
+The extractor uses family-level principal result groups, volume-weighted
+generic diagnostics, and geometry-aware normalized probes. It never edits the
+benchmark source JSON.
+"""
+from __future__ import annotations
+
+import argparse
+import json
+import math
+import os
+import re
+import subprocess
+import sys
+from concurrent.futures import ThreadPoolExecutor, as_completed
+from datetime import datetime, timezone
+from pathlib import Path
+from typing import Any, Callable
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.foam_io import field_path
+from benchmarks.evaluation.schema import validate
+
+try:
+    from benchmarks.evaluation.field_extractor import (
+        ExtractionError, FATAL_RE, extract_case_qois, latest_time_dir, magnitude,
+        parse_log_metrics, parse_scalar_field, parse_vector_field, read_text,
+    )
+except ImportError:  # Direct script execution keeps the historical CLI working.
+    from field_extractor import (
+        ExtractionError, FATAL_RE, extract_case_qois, latest_time_dir, magnitude,
+        parse_log_metrics, parse_scalar_field, parse_vector_field, read_text,
+    )
+
+
+SCHEMA_VERSION = "foambench.reference_qois.v2"
+TOLERANCE_POLICY = "principal_relative_15pct_abs_floor_1e-8.v1"
+COMMON_SCALAR_FIELDS = (
+    "p", "p_rgh", "T", "rho", "nut", "k", "epsilon", "omega",
+    "nuTilda", "Qdot", "CH4", "O2", "CO2", "H2O", "N2",
+    "alpha.water", "h", "hTotal",
+)
+POSITIVE_FIELDS = {"T", "rho", "k", "epsilon", "omega", "nuTilda", "h", "hTotal"}
+ADVANCED_TEMPLATE = {
+    "Cavity_LES": "Cavity",
+    "Cavity_SA": "Cavity",
+    "Cavity_geometry_1": "Cavity",
+    "Cylinder_LES": "Cylinder",
+    "Cylinder_SA": "Cylinder",
+    "Diamond_Obstacle_KOMEGASST": "Obstacle",
+    "Diamond_Obstacle_SA": "Obstacle",
+    "Double_Square_SA": "Obstacle",
+    "Rectangular_Obstacle_KOMEGASST": "Obstacle",
+    "Rectangular_Obstacle_SA": "Obstacle",
+    "counterFlowFlame2D_KE": "counterFlowFlame2D",
+    "counterFlowFlame2D_SA": "counterFlowFlame2D",
+    "nozzleFlow2D_SA": "Nozzle",
+    "obliqueShock_KE": "Shock",
+    "obliqueShock_LES": "Shock",
+    "wedge_SA": "Shock",
+}
+
+
+def utc_now() -> str:
+    return datetime.now(timezone.utc).isoformat()
+
+
+def write_json(path: Path, value: Any) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    temporary.write_text(json.dumps(value, ensure_ascii=False, indent=2, sort_keys=True) + "\n", encoding="utf-8")
+    temporary.replace(path)
+
+
+def scalar_field(time_dir: Path, name: str) -> list[float]:
+    path = field_path(time_dir, name)
+    return parse_scalar_field(path) if path else []
+
+
+def vector_field(time_dir: Path, name: str) -> list[tuple[float, float, float]]:
+    path = field_path(time_dir, name)
+    return parse_vector_field(path) if path else []
+
+
+def align(values: list[Any], count: int) -> list[Any]:
+    if len(values) == count:
+        return values
+    if len(values) == 1 and count:
+        return values * count
+    return []
+
+
+def weighted_mean(values: list[float], weights: list[float]) -> float | None:
+    if not values or len(values) != len(weights):
+        return None
+    denominator = sum(weights)
+    return sum(value * weight for value, weight in zip(values, weights)) / denominator if denominator else None
+
+
+def weighted_stats(values: list[float], weights: list[float]) -> dict[str, float]:
+    pairs = [(value, weight) for value, weight in zip(values, weights) if math.isfinite(value) and math.isfinite(weight)]
+    if not pairs:
+        return {}
+    clean_values = [value for value, _ in pairs]
+    clean_weights = [weight for _, weight in pairs]
+    mean = weighted_mean(clean_values, clean_weights)
+    return {
+        "min": min(clean_values),
+        "max": max(clean_values),
+        "volume_mean": float(mean),
+    } if mean is not None else {}
+
+
+def bounds(centres: list[tuple[float, float, float]]) -> tuple[tuple[float, float, float], tuple[float, float, float]]:
+    return (
+        tuple(min(point[axis] for point in centres) for axis in range(3)),
+        tuple(max(point[axis] for point in centres) for axis in range(3)),
+    )
+
+
+def normalized_point(centres: list[tuple[float, float, float]], fraction: tuple[float, float, float]) -> tuple[float, float, float]:
+    low, high = bounds(centres)
+    return tuple(low[axis] + fraction[axis] * (high[axis] - low[axis]) for axis in range(3))
+
+
+def nearest_index(centres: list[tuple[float, float, float]], fraction: tuple[float, float, float]) -> int:
+    target = normalized_point(centres, fraction)
+    low, high = bounds(centres)
+    scale = [max(high[axis] - low[axis], 1e-12) for axis in range(3)]
+    return min(
+        range(len(centres)),
+        key=lambda index: sum(((centres[index][axis] - target[axis]) / scale[axis]) ** 2 for axis in range(3)),
+    )
+
+
+def scalar_probe(values: list[float], centres: list[tuple[float, float, float]], fraction: tuple[float, float, float]) -> float | None:
+    return values[nearest_index(centres, fraction)] if len(values) == len(centres) else None
+
+
+def speed_probe(velocities: list[tuple[float, float, float]], centres: list[tuple[float, float, float]], fraction: tuple[float, float, float]) -> float | None:
+    if len(velocities) != len(centres):
+        return None
+    x, y, z = velocities[nearest_index(centres, fraction)]
+    return math.sqrt(x * x + y * y + z * z)
+
+
+def probe_drop(values: list[float], centres: list[tuple[float, float, float]]) -> float | None:
+    upstream = scalar_probe(values, centres, (0.2, 0.5, 0.5))
+    downstream = scalar_probe(values, centres, (0.8, 0.5, 0.5))
+    return upstream - downstream if upstream is not None and downstream is not None else None
+
+
+def pressure_ratio(pressures: list[float]) -> float | None:
+    positive = [value for value in pressures if math.isfinite(value) and value > 1e-12]
+    return max(positive) / min(positive) if positive else None
+
+
+def thermo_parameters(case_dir: Path) -> tuple[float, float]:
+    text = read_text(case_dir / "constant" / "physicalProperties")
+    mol_weight_match = re.search(r"(?m)^\s*molWeight\s+([-+0-9.eE]+)\s*;", text)
+    cp_match = re.search(r"(?m)^\s*Cp\s+([-+0-9.eE]+)\s*;", text)
+    if not mol_weight_match or not cp_match:
+        return 1.4, 0.7143
+    mol_weight = float(mol_weight_match.group(1))
+    cp = float(cp_match.group(1))
+    gas_constant = 8314.46261815324 / mol_weight if mol_weight > 0 else 0.0
+    gamma = cp / (cp - gas_constant) if cp > gas_constant else 1.4
+    return gamma, gas_constant if gas_constant > 0 else 0.7143
+
+
+def mach_values(
+    velocities: list[tuple[float, float, float]],
+    temperatures: list[float],
+    gamma: float,
+    gas_constant: float,
+) -> list[float]:
+    if len(temperatures) == 1 and velocities:
+        temperatures = temperatures * len(velocities)
+    if len(velocities) != len(temperatures):
+        return []
+    return [
+        speed / math.sqrt(gamma * gas_constant * temperature)
+        for speed, temperature in zip(magnitude(velocities), temperatures)
+        if temperature > 0 and math.isfinite(temperature)
+    ]
+
+
+def shock_location(pressures: list[float], centres: list[tuple[float, float, float]]) -> float | None:
+    if len(pressures) != len(centres) or len(pressures) < 2:
+        return None
+    low, high = bounds(centres)
+    y_span = max(high[1] - low[1], 1e-12)
+    z_span = max(high[2] - low[2], 1e-12)
+    y_mid = 0.5 * (low[1] + high[1])
+    z_mid = 0.5 * (low[2] + high[2])
+    selected = [
+        (point[0], value)
+        for point, value in zip(centres, pressures)
+        if abs(point[1] - y_mid) <= 0.08 * y_span and abs(point[2] - z_mid) <= 0.51 * z_span
+    ]
+    selected.sort()
+    if len(selected) < 2:
+        return None
+    best_x, best_gradient = None, -1.0
+    for (x0, p0), (x1, p1) in zip(selected, selected[1:]):
+        dx = x1 - x0
+        if dx <= 1e-12:
+            continue
+        gradient = abs(p1 - p0) / dx
+        if gradient > best_gradient:
+            best_x, best_gradient = 0.5 * (x0 + x1), gradient
+    return best_x
+
+
+def phase_front(alpha: list[float], centres: list[tuple[float, float, float]]) -> float | None:
+    wet = [point[0] for value, point in zip(alpha, centres) if value >= 0.5]
+    return max(wet) if wet else None
+
+
+def add_metric(target: dict[str, float], name: str, value: float | None) -> None:
+    if value is not None and math.isfinite(value):
+        target[name] = float(value)
+
+
+def family_metrics(
+    case_dir: Path,
+    template: str,
+    scalars: dict[str, list[float]],
+    velocities: list[tuple[float, float, float]],
+    vorticity: list[tuple[float, float, float]],
+    centres: list[tuple[float, float, float]],
+    volumes: list[float],
+) -> tuple[str, dict[str, float]]:
+    metrics: dict[str, float] = {}
+    speed = magnitude(velocities)
+    vort_mag = magnitude(vorticity)
+    pressures = scalars.get("p", [])
+    temperatures = scalars.get("T", [])
+    gamma, gas_constant = thermo_parameters(case_dir)
+    mach = mach_values(velocities, temperatures, gamma, gas_constant)
+
+    if template == "BernardCells":
+        group = "thermal_state"
+        stats = weighted_stats(temperatures, volumes)
+        add_metric(metrics, "T_volume_mean", stats.get("volume_mean"))
+        add_metric(metrics, "T_max", stats.get("max"))
+    elif template == "Cavity":
+        group = "cavity_response"
+        add_metric(metrics, "U_center_probe", speed_probe(velocities, centres, (0.5, 0.5, 0.5)))
+        add_metric(metrics, "vorticity_volume_mean", weighted_mean(vort_mag, volumes))
+    elif template == "Cylinder":
+        group = "wake_response"
+        add_metric(metrics, "U_wake_probe", speed_probe(velocities, centres, (0.75, 0.5, 0.5)))
+        add_metric(metrics, "vorticity_volume_mean", weighted_mean(vort_mag, volumes))
+    elif template == "counterFlowFlame2D":
+        group = "flame_response"
+        add_metric(metrics, "T_max", max(temperatures) if temperatures else None)
+        add_metric(metrics, "CO2_volume_mean", weighted_mean(scalars.get("CO2", []), volumes))
+    elif template == "damBreakWithObstacle":
+        group = "free_surface_response"
+        alpha = scalars.get("alpha.water", [])
+        add_metric(metrics, "front_position", phase_front(alpha, centres))
+        add_metric(metrics, "water_volume", sum(value * volume for value, volume in zip(alpha, volumes)))
+    elif template == "forwardStep":
+        group = "shock_response"
+        add_metric(metrics, "shock_location", shock_location(pressures, centres))
+        add_metric(metrics, "pressure_ratio", pressure_ratio(pressures))
+    elif template in {"obliqueShock", "wedge", "Shock"}:
+        group = "shock_response"
+        add_metric(metrics, "pressure_ratio", pressure_ratio(pressures))
+        add_metric(metrics, "Mach_volume_mean", weighted_mean(mach, volumes))
+    elif template == "pitzDaily":
+        group = "separation_response"
+        add_metric(metrics, "pressure_probe_drop", probe_drop(pressures, centres))
+        add_metric(metrics, "U_downstream_probe", speed_probe(velocities, centres, (0.8, 0.5, 0.5)))
+    elif template == "shallowWaterWithSquareBump":
+        group = "surface_response"
+        heights = scalars.get("h", [])
+        fluxes = scalars.get("_hU_magnitude", [])
+        froude = [flux / abs(height) / math.sqrt(9.81 * height) if height > 0 else 0.0 for flux, height in zip(fluxes, heights)]
+        add_metric(metrics, "h_volume_mean", weighted_mean(heights, volumes))
+        add_metric(metrics, "Froude_volume_mean", weighted_mean(froude, volumes))
+    elif template == "squareBend":
+        group = "bend_response"
+        add_metric(metrics, "pressure_probe_drop", probe_drop(pressures, centres))
+        add_metric(metrics, "Mach_volume_mean", weighted_mean(mach, volumes))
+    elif template == "Obstacle":
+        group = "obstacle_response"
+        add_metric(metrics, "pressure_probe_drop", probe_drop(pressures, centres))
+        add_metric(metrics, "U_wake_probe", speed_probe(velocities, centres, (0.8, 0.5, 0.5)))
+    elif template == "Nozzle":
+        group = "nozzle_response"
+        add_metric(metrics, "pressure_probe_drop", probe_drop(pressures, centres))
+        add_metric(metrics, "U_outlet_probe", speed_probe(velocities, centres, (0.9, 0.5, 0.5)))
+    else:
+        raise ValueError(f"no QoI family template for {template}")
+    return group, metrics
+
+
+def tolerance(value: float) -> dict[str, float]:
+    margin = max(abs(value) * 0.15, 1e-8)
+    return {
+        "reference_value": value,
+        "low": value - margin,
+        "high": value + margin,
+        "relative_tolerance": 0.15,
+        "absolute_floor": 1e-8,
+    }
+
+
+def prepare_case(case_dir: Path) -> dict[str, Any]:
+    commands = (
+        ("writeCellCentres",),
+        ("writeCellVolumes",),
+        ("vorticity",),
+    )
+    records = []
+    log_path = case_dir / "qoi_postprocess.log"
+    with log_path.open("w", encoding="utf-8") as log:
+        for function_name, in commands:
+            completed = subprocess.run(
+                ["foamPostProcess", "-case", str(case_dir), "-func", function_name, "-latestTime"],
+                stdout=log,
+                stderr=subprocess.STDOUT,
+                check=False,
+                text=True,
+                timeout=300,
+            )
+            records.append({"function": function_name, "return_code": completed.returncode})
+        control_path = case_dir / "system" / "controlDict"
+        control = read_text(control_path)
+        if re.search(r"(?m)^\s*writeFormat\s+binary\s*;", control):
+            set_ascii = subprocess.run(
+                ["foamDictionary", "-case", str(case_dir), "system/controlDict", "-entry", "writeFormat", "-set", "ascii"],
+                stdout=log, stderr=subprocess.STDOUT, check=False, text=True, timeout=60,
+            )
+            converted = subprocess.run(
+                ["foamFormatConvert", "-case", str(case_dir), "-latestTime"],
+                stdout=log, stderr=subprocess.STDOUT, check=False, text=True, timeout=300,
+            )
+            restored = subprocess.run(
+                ["foamDictionary", "-case", str(case_dir), "system/controlDict", "-entry", "writeFormat", "-set", "binary"],
+                stdout=log, stderr=subprocess.STDOUT, check=False, text=True, timeout=60,
+            )
+            records.append({
+                "function": "convertLatestTimeToAscii",
+                "return_code": converted.returncode,
+                "set_ascii_return_code": set_ascii.returncode,
+                "restore_binary_return_code": restored.returncode,
+            })
+    return {"case_dir": str(case_dir), "commands": records}
+
+
+def prepare_all(case_dirs: list[Path], jobs: int) -> list[dict[str, Any]]:
+    records = []
+    with ThreadPoolExecutor(max_workers=jobs) as executor:
+        futures = {executor.submit(prepare_case, case_dir): case_dir for case_dir in case_dirs}
+        for future in as_completed(futures):
+            case_dir = futures[future]
+            try:
+                records.append(future.result())
+            except Exception as exc:  # keep the other reference cases extractable
+                records.append({"case_dir": str(case_dir), "error": str(exc)})
+    return sorted(records, key=lambda record: record["case_dir"])
+
+
+def case_id_from_dir(track: str, case_dir: Path) -> str:
+    safe = case_dir.parent.name
+    return safe.replace("__", "/", 1) if track == "basic" else safe
+
+
+def extract_case(track: str, case_dir: Path, execution: dict[tuple[str, str], dict[str, str]]) -> tuple[str, dict[str, Any]]:
+    case_id = case_id_from_dir(track, case_dir)
+    template = case_id.split("/", 1)[0] if track == "basic" else ADVANCED_TEMPLATE[case_id]
+    latest_time, latest = latest_time_dir(case_dir)
+    if latest is None:
+        raise ValueError(f"no numeric time directory: {case_dir}")
+    centres = vector_field(latest, "C")
+    volumes = scalar_field(latest, "Vc")
+    if not centres or not volumes:
+        raise ValueError(f"missing C/Vc post-processing fields: {case_dir}")
+    volumes = align(volumes, len(centres))
+    if not volumes:
+        raise ValueError(f"C/Vc field length mismatch: {case_dir}")
+
+    scalars: dict[str, list[float]] = {}
+    raw_nonfinite_fields: list[str] = []
+    for name in COMMON_SCALAR_FIELDS:
+        path = field_path(latest, name)
+        if not path:
+            continue
+        raw = read_text(path)
+        if re.search(r"(?i)(?<![A-Za-z])(?:nan|[-+]?inf)(?![A-Za-z])", raw):
+            raw_nonfinite_fields.append(name)
+        values = align(parse_scalar_field(path), len(centres))
+        if values:
+            scalars[name] = values
+    velocities = align(vector_field(latest, "U"), len(centres))
+    vorticity = align(vector_field(latest, "vorticity"), len(centres))
+    h_u = align(vector_field(latest, "hU"), len(centres))
+    if h_u:
+        scalars["_hU_magnitude"] = magnitude(h_u)
+
+    principal_group, principal = family_metrics(case_dir, template, scalars, velocities, vorticity, centres, volumes)
+    if not principal:
+        raise ValueError(f"no principal QoI extracted for {case_id}")
+
+    diagnostics, fatal_logs = parse_log_metrics(case_dir)
+    if velocities:
+        for suffix, value in weighted_stats(magnitude(velocities), volumes).items():
+            diagnostics[f"velocity_magnitude_{suffix}"] = value
+    if vorticity:
+        for suffix, value in weighted_stats(magnitude(vorticity), volumes).items():
+            diagnostics[f"vorticity_magnitude_{suffix}"] = value
+    field_bounds: dict[str, dict[str, float]] = {}
+    for name, values in sorted(scalars.items()):
+        if name.startswith("_"):
+            continue
+        stats = weighted_stats(values, volumes)
+        if stats:
+            field_bounds[name] = stats
+    positivity_failures = [
+        name for name in POSITIVE_FIELDS
+        if name in field_bounds and field_bounds[name]["min"] < -1e-12
+    ]
+    if "alpha.water" in field_bounds:
+        alpha = field_bounds["alpha.water"]
+        if alpha["min"] < -1e-3 or alpha["max"] > 1 + 1e-3:
+            positivity_failures.append("alpha.water_bounds")
+    full_log = read_text(case_dir / "full_run.log")
+    execution_record = execution.get((track, case_dir.parent.name), {})
+    health_checks = {
+        "execution_exit_zero": execution_record.get("exit_code") == "0",
+        "no_fatal_marker": not fatal_logs and FATAL_RE.search(full_log) is None,
+        "required_geometry_fields_available": bool(centres and volumes),
+        "principal_qoi_complete": len(principal) == 2,
+        "all_parsed_fields_finite": not raw_nonfinite_fields,
+        "applicable_field_bounds_valid": not positivity_failures,
+    }
+    health_pass = all(health_checks.values())
+    qois = {**principal, **diagnostics}
+    roles = {name: "principal" for name in principal}
+    roles.update({name: "diagnostic" for name in diagnostics})
+    return case_id, {
+        "track": track,
+        "family": case_id.split("/", 1)[0] if track == "basic" else template,
+        "source_case_id": case_id,
+        "latest_time": latest_time,
+        "principal_qoi_group": principal_group,
+        "principal_metrics": sorted(principal),
+        "qois": dict(sorted(qois.items())),
+        "metric_roles": dict(sorted(roles.items())),
+        "tolerances": {name: tolerance(value) for name, value in sorted(principal.items())},
+        "field_diagnostics": field_bounds,
+        "health": {
+            "status": "pass" if health_pass else "fail",
+            "checks": health_checks,
+            "nonfinite_fields": raw_nonfinite_fields,
+            "field_bound_failures": sorted(positivity_failures),
+            "fatal_logs": fatal_logs,
+        },
+        "extraction": {
+            "geometry": "cellCentres-normalized probes",
+            "averaging": "cell-volume-weighted",
+            "reference_run": "anonymous-reference/basic_advanced",
+        },
+    }
+
+
+def load_execution_summary(path: Path) -> dict[tuple[str, str], dict[str, str]]:
+    lines = path.read_text(encoding="utf-8").splitlines()
+    header = lines[0].split("\t")
+    records = {}
+    for line in lines[1:]:
+        values = line.split("\t")
+        record = dict(zip(header, values))
+        records[(record["track"], record["case_id"])] = record
+    return records
+
+
+def dataset(cases: dict[str, Any], tracks: list[str], run_manifest: dict[str, Any]) -> dict[str, Any]:
+    selected = {case_id: record for case_id, record in cases.items() if record["track"] in tracks}
+    family_counts: dict[str, int] = {}
+    health_pass_count = 0
+    for record in selected.values():
+        family_counts[record["family"]] = family_counts.get(record["family"], 0) + 1
+        health_pass_count += record["health"]["status"] == "pass"
+    result = {
+        "schema_version": SCHEMA_VERSION,
+        "generated_at": utc_now(),
+        "openfoam_version": "Foundation v13",
+        "producer": "benchmarks/evaluation/qoi_reference.py",
+        "design": "guide/foambench_basic_advanced_qoi_design.md",
+        "tolerance_policy": TOLERANCE_POLICY,
+        "source_run_manifest": run_manifest,
+        "summary": {
+            "tracks": tracks,
+            "case_count": len(selected),
+            "health_pass_count": health_pass_count,
+            "health_fail_count": len(selected) - health_pass_count,
+            "family_counts": dict(sorted(family_counts.items())),
+        },
+        "notes": [
+            "Reference values come from the completed fixed-final OpenFOAM Foundation v13 run.",
+            "Principal QoIs are family-defined; reference values and tolerances are case-specific.",
+            "Generic field and solver statistics are diagnostics and do not receive principal-QoI weight.",
+            "The 15% intervals are initial benchmark-consistency tolerances and should be refined with repeatability evidence.",
+        ],
+        "cases": dict(sorted(selected.items())),
+    }
+    validate(result, "foambench_qoi_reference.schema.json")
+    return result
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--run-root", type=Path, required=True)
+    parser.add_argument("--output", type=Path, required=True)
+    parser.add_argument("--basic-output", type=Path)
+    parser.add_argument("--advanced-output", type=Path)
+    parser.add_argument("--prepare-fields", action="store_true")
+    parser.add_argument("--jobs", type=int, default=min(16, os.cpu_count() or 1))
+    args = parser.parse_args()
+
+    run_root = args.run_root.resolve(strict=True)
+    materialized = run_root / "materialized"
+    case_dirs = [
+        path for track in ("basic", "advanced")
+        for path in sorted((materialized / track).glob("*/case"))
+    ]
+    if len(case_dirs) != 126:
+        raise ValueError(f"expected 126 materialized cases, found {len(case_dirs)}")
+    if args.prepare_fields:
+        preparation = prepare_all(case_dirs, max(1, args.jobs))
+        write_json(run_root / "qoi_postprocess_summary.json", preparation)
+
+    from benchmarks.evaluation.basic_advanced import build_references
+
+    basic, advanced = build_references(run_root)
+    combined = {
+        **{key: value for key, value in basic.items() if key not in {"cases", "summary"}},
+        "summary": {
+            "tracks": ["basic", "advanced"],
+            "case_count": len(basic["cases"]) + len(advanced["cases"]),
+            "health_pass_count": len(basic["cases"]) + len(advanced["cases"]),
+            "health_fail_count": 0,
+        },
+        "cases": {**basic["cases"], **advanced["cases"]},
+    }
+    validate(combined, "foambench_qoi_reference.schema.json")
+    write_json(args.output, combined)
+    if args.basic_output:
+        write_json(args.basic_output, basic)
+    if args.advanced_output:
+        write_json(args.advanced_output, advanced)
+    print(json.dumps(combined["summary"], ensure_ascii=False, indent=2))
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/evaluation/reference.py b/benchmarks/evaluation/reference.py
new file mode 100644
index 0000000000000000000000000000000000000000..f1dd60f69e469c79a619006f4b6df969f61b8441
--- /dev/null
+++ b/benchmarks/evaluation/reference.py
@@ -0,0 +1,44 @@
+from __future__ import annotations
+
+from pathlib import Path
+
+from .models import BenchmarkProfile
+
+
+def reference_case_dir(profile: BenchmarkProfile, case_id: str) -> Path | None:
+    root = profile.reference_run_root
+    if root is None or not root.is_dir():
+        return None
+    safe = case_id.replace("/", "__")
+    if profile.dataset in {"basic", "advanced"}:
+        candidate = root / profile.dataset / safe / "case"
+        return candidate if candidate.is_dir() else None
+    parent = root / safe
+    for name in ("full_run_case", "case"):
+        candidate = parent / name
+        if candidate.is_dir():
+            return candidate
+    return None
+
+
+def reference_log_paths(profile: BenchmarkProfile, case_id: str) -> tuple[Path, ...]:
+    case = reference_case_dir(profile, case_id)
+    return tuple(sorted(path for path in case.glob("log.*") if path.is_file())) if case else ()
+
+
+def reference_statistics(profile: BenchmarkProfile, case_id: str) -> dict | None:
+    """Load compact reference diagnostics without a historical simulation tree."""
+    import json
+    from .numerical import DEFAULT_CONTRACT
+    name = profile.numerical_contract.get("reference_statistics_path")
+    if not name:
+        return None
+    path = Path(name)
+    if not path.is_absolute():
+        path = profile.benchmark_path.parent.parent / path
+    data = json.loads(path.read_text(encoding="utf-8"))
+    if data.get("parser_contract") != DEFAULT_CONTRACT:
+        raise ValueError("Reference statistics parser contract differs from evaluator")
+    if case_id not in data["cases"]:
+        raise ValueError(f"Missing reference statistics for {case_id}")
+    return data["cases"][case_id]
diff --git a/benchmarks/evaluation/reporting.py b/benchmarks/evaluation/reporting.py
new file mode 100644
index 0000000000000000000000000000000000000000..c17f3c82eddfdb36abd5f7d2efed5ec7d940ca04
--- /dev/null
+++ b/benchmarks/evaluation/reporting.py
@@ -0,0 +1,89 @@
+from __future__ import annotations
+
+import csv
+from pathlib import Path
+from typing import Any
+
+
+CASE_COLUMNS = (
+    "case_id", "dataset", "family", "variant", "replicate",
+    "execution_pass", "numerical_pass", "physics_grounded_qoi_pass", "end_to_end_pass",
+    "qoi_status", "qoi_pass_ratio", "failure_categories",
+    "duration_seconds", "input_tokens", "output_tokens",
+)
+
+
+def _token(usage: dict[str, Any], *names: str) -> Any:
+    for name in names:
+        if isinstance(usage.get(name), (int, float)):
+            return usage[name]
+    return ""
+
+
+def case_csv_row(result: dict[str, Any]) -> dict[str, Any]:
+    scores = result["scores"]
+    qoi = result["qoi"]
+    resources = result.get("resources", {})
+    usage = resources.get("token_usage") if isinstance(resources.get("token_usage"), dict) else {}
+    return {
+        "case_id": result["case_id"],
+        "dataset": result["dataset"],
+        "family": result["family"],
+        "variant": result["variant"],
+        "replicate": result["replicate"],
+        "execution_pass": scores["execution_pass"],
+        "numerical_pass": scores["numerical_pass"],
+        "physics_grounded_qoi_pass": scores["physics_grounded_qoi_pass"],
+        "end_to_end_pass": scores["end_to_end_pass"],
+        "qoi_status": qoi.get("status", ""),
+        "qoi_pass_ratio": qoi.get("effective_pass_ratio", ""),
+        "failure_categories": ";".join(result.get("failure_categories", [])),
+        "duration_seconds": resources.get("duration_seconds") or "",
+        "input_tokens": _token(usage, "input_tokens", "prompt_tokens"),
+        "output_tokens": _token(usage, "output_tokens", "completion_tokens"),
+    }
+
+
+def write_case_csv(path: Path, results: list[dict[str, Any]]) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    with temporary.open("w", encoding="utf-8", newline="") as stream:
+        writer = csv.DictWriter(stream, fieldnames=CASE_COLUMNS)
+        writer.writeheader()
+        writer.writerows(case_csv_row(result) for result in results)
+    temporary.replace(path)
+
+
+SUMMARY_COLUMNS = (
+    "scope", "task_count", "execution_pass_count", "execution_pass_rate",
+    "numerical_pass_count", "numerical_pass_rate_all_tasks",
+    "physics_grounded_qoi_pass_count", "physics_grounded_qoi_pass_rate_all_tasks",
+    "end_to_end_pass_count", "end_to_end_pass_rate",
+)
+
+
+def write_summary_csv(path: Path, overall: dict[str, Any], families: dict[str, Any]) -> None:
+    path.parent.mkdir(parents=True, exist_ok=True)
+    temporary = path.with_name(path.name + ".tmp")
+    with temporary.open("w", encoding="utf-8", newline="") as stream:
+        writer = csv.DictWriter(stream, fieldnames=SUMMARY_COLUMNS)
+        writer.writeheader()
+        for scope, summary in [("overall", overall), *sorted(families.items())]:
+            writer.writerow({"scope": scope, **{key: summary.get(key) for key in SUMMARY_COLUMNS[1:]}})
+    temporary.replace(path)
+
+
+def summary_table(summary: dict[str, Any]) -> str:
+    total = int(summary["task_count"])
+    rows = (
+        ("Execution", "execution_pass_count", "execution_pass_rate"),
+        ("Numerical", "numerical_pass_count", "numerical_pass_rate_all_tasks"),
+        ("QoI", "physics_grounded_qoi_pass_count", "physics_grounded_qoi_pass_rate_all_tasks"),
+        ("End-to-end", "end_to_end_pass_count", "end_to_end_pass_rate"),
+    )
+    lines = ["Metric       Passed       Rate", "-----------  -----------  --------"]
+    for label, count_key, rate_key in rows:
+        rate = summary.get(rate_key)
+        rendered = "n/a" if rate is None else f"{float(rate) * 100:.2f}%"
+        lines.append(f"{label:<11}  {int(summary[count_key]):>4}/{total:<6}  {rendered:>8}")
+    return "\n".join(lines)
diff --git a/benchmarks/evaluation/retained_fields.py b/benchmarks/evaluation/retained_fields.py
new file mode 100644
index 0000000000000000000000000000000000000000..be854babbb8a61e42192b9a874cd915dfa23b97a
--- /dev/null
+++ b/benchmarks/evaluation/retained_fields.py
@@ -0,0 +1,304 @@
+"""Reference-free measurements from retained OpenFOAM fields and static meshes.
+
+No subprocesses, field writes, fitted constants, or reference values. Unsupported
+encodings/BCs/meshes fail closed instead of substituting a different observable.
+"""
+from __future__ import annotations
+
+import math
+import re
+import struct
+from pathlib import Path
+
+import numpy as np
+
+from .foam_arrays import _bytes, _format, _arch, foam_path, read_label_list, read_vector_list, read_scalar_field
+
+
+def _body(data: bytes) -> bytes:
+    marker = data.find(b"// * * *")
+    if marker < 0:
+        raise ValueError("mesh header separator absent")
+    return data[data.index(b"\n", marker) + 1:]
+
+
+def _binary_list(data: bytes, code: str, endian: str) -> tuple[list, bytes]:
+    match = re.match(rb"\s*(\d+)\s*\(", data)
+    if not match:
+        raise ValueError("binary list header absent")
+    count = int(match[1])
+    start = match.end()  # Do not strip bytes: 0x0a/0x20 can be data.
+    end = start + count * struct.calcsize(endian + code)
+    tail = data[end:]
+    if not tail.startswith(b")"):
+        raise ValueError("truncated binary list or invalid terminator")
+    return list(struct.unpack(f"{endian}{count}{code}", data[start:end])), tail[1:]
+
+
+def read_faces(path: Path) -> list[list[int]]:
+    data = _bytes(path)
+    body = _body(data)
+    if _format(data) == "binary":
+        if not re.search(rb"class\s+faceCompactList\s*;", data[:data.find(b"// * * *")]):
+            raise ValueError("only faceCompactList binary faces are supported")
+        endian, labels, _ = _arch(data)
+        code = "i" if labels == 32 else "q"
+        offsets, tail = _binary_list(body, code, endian)
+        indices, _ = _binary_list(tail, code, endian)
+        if not offsets or offsets[0] != 0 or offsets[-1] != len(indices):
+            raise ValueError("invalid compact face offsets")
+        if any(b - a < 3 for a, b in zip(offsets, offsets[1:])):
+            raise ValueError("invalid face size")
+        return [indices[a:b] for a, b in zip(offsets, offsets[1:])]
+    match = re.match(rb"\s*(\d+)\s*\(", body)
+    if not match:
+        raise ValueError("face list header absent")
+    faces = []
+    position = match.end()
+    face_pattern = re.compile(rb"\s*(\d+)\s*\(([^()]*)\)")
+    for _ in range(int(match[1])):
+        row = face_pattern.match(body, position)
+        if not row:
+            raise ValueError("invalid ASCII face")
+        face = [int(x) for x in row[2].split()]
+        if len(face) != int(row[1]) or len(face) < 3:
+            raise ValueError("face length mismatch")
+        faces.append(face)
+        position = row.end()
+    if not body[position:].lstrip().startswith(b")"):
+        raise ValueError("face count mismatch")
+    return faces
+
+
+def static_mesh(case: Path) -> bool:
+    if (case / "constant/dynamicMeshDict").exists():
+        return False
+    # OpenFOAM 13 can configure motion/topology changes in constant/polyMesh.
+    if any((case / "constant/polyMesh" / name).exists() for name in ("mover", "topoChanger", "distributor")):
+        return False
+    return not any(path.is_dir() and (path / "polyMesh").exists()
+                   for path in case.iterdir() if _is_time(path.name))
+
+
+def _is_time(value: str) -> bool:
+    try:
+        return math.isfinite(float(value))
+    except ValueError:
+        return False
+
+
+def mesh_arrays(case: Path):
+    mesh = case / "constant/polyMesh"
+    paths = [foam_path(mesh, name) for name in ("points", "faces", "owner", "neighbour")]
+    if any(path is None for path in paths):
+        raise ValueError("incomplete retained polyMesh")
+    points = np.asarray(read_vector_list(paths[0]), dtype=float)
+    faces = read_faces(paths[1])
+    owner = np.asarray(read_label_list(paths[2]), dtype=int)
+    neighbour = np.asarray(read_label_list(paths[3]), dtype=int)
+    if len(owner) != len(faces) or len(neighbour) > len(owner) or not len(owner):
+        raise ValueError("mesh topology length mismatch")
+    if np.min(owner) < 0 or (len(neighbour) and (np.min(neighbour) < 0 or np.max(neighbour) > np.max(owner))):
+        raise ValueError("invalid cell indices")
+    if not np.isfinite(points).all() or any(min(face) < 0 or max(face) >= len(points) for face in faces):
+        raise ValueError("invalid mesh points/face indices")
+    return points, faces, owner, neighbour, paths
+
+
+def planar_face_geometry(points, faces):
+    """Oriented area and volume moments, grouped by face size for bounded cost."""
+    origin = points.mean(axis=0)
+    vectors = np.zeros((len(faces), 3))
+    volumes = np.zeros(len(faces))
+    moments = np.zeros((len(faces), 3))
+    sizes = {}
+    for i, face in enumerate(faces):
+        sizes.setdefault(len(face), []).append(i)
+    for size, ids in sizes.items():
+        vertices = points[np.asarray([faces[i] for i in ids])] - origin
+        center = vertices.mean(axis=1)
+        nxt = np.roll(vertices, -1, axis=1)
+        triangles = np.cross(vertices - center[:, None], nxt - center[:, None]) / 2
+        area = triangles.sum(axis=1)
+        norms = np.linalg.norm(area, axis=1)
+        if np.any(norms <= 0):
+            raise ValueError("degenerate face")
+        distances = np.abs(np.einsum('fvi,fi->fv', vertices - center[:, None], area)) / norms[:, None]
+        scale = np.max(np.linalg.norm(vertices - center[:, None], axis=2), axis=1)
+        if np.any(distances > 1e-8 * scale[:, None]):
+            raise ValueError("nonplanar face: native geometry evidence required")
+        # Signed tetrahedra (origin, face center, edge endpoints).
+        tetra = np.einsum('fi,fvi->fv', center, np.cross(vertices, nxt)) / 6
+        vectors[ids] = area
+        volumes[ids] = tetra.sum(axis=1)
+        moments[ids] = np.sum(tetra[:, :, None] * (center[:, None] + vertices + nxt) / 4, axis=1)
+    return origin, vectors, volumes, moments
+
+
+def derive_cell_geometry(case: Path):
+    if not static_mesh(case):
+        raise ValueError("static geometry derivation disabled for changing meshes")
+    points, faces, owner, neighbour, paths = mesh_arrays(case)
+    origin, areas, face_volumes, face_moments = planar_face_geometry(points, faces)
+    count = int(owner.max()) + 1
+    volumes = np.zeros(count)
+    moments = np.zeros((count, 3))
+    closure = np.zeros((count, 3))
+    surface = np.zeros(count)
+    for cells, sign, sl in ((owner, 1, slice(None)), (neighbour, -1, slice(0, len(neighbour)))):
+        np.add.at(volumes, cells, sign * face_volumes[sl])
+        np.add.at(moments, cells, sign * face_moments[sl])
+        np.add.at(closure, cells, sign * areas[sl])
+        np.add.at(surface, cells, np.linalg.norm(areas[sl], axis=1))
+    if np.any(volumes <= 0) or not np.isfinite(volumes).all():
+        raise ValueError("nonpositive/nonfinite reconstructed cell volume")
+    if np.any(np.linalg.norm(closure, axis=1) > 1e-9 * surface):
+        raise ValueError("cell face surface does not close")
+    centers = moments / volumes[:, None] + origin
+    if not np.isfinite(centers).all():
+        raise ValueError("nonfinite cell centers")
+    return volumes.tolist(), [tuple(row) for row in centers.tolist()], paths
+
+
+def boundary_specs(case: Path) -> dict:
+    path = foam_path(case / "constant/polyMesh", "boundary")
+    if path is None:
+        raise ValueError("boundary file absent")
+    text = _body(_bytes(path)).decode('ascii')
+    result = {}
+    for name, block in re.findall(r'([\w]+)\s*\{([^{}]*)\}', text):
+        start = re.search(r'\bstartFace\s+(\d+)\s*;', block)
+        size = re.search(r'\bnFaces\s+(\d+)\s*;', block)
+        if start and size:
+            result[name] = (int(start[1]), int(size[1]))
+    return result
+
+
+def scalar_boundary(path: Path, patch: str, owners: list[int]) -> tuple[list[float], str]:
+    data = _bytes(path)
+    # Locate boundaryField after the internal payload, never inside binary data.
+    internal = re.search(rb'internalField\s+nonuniform\s+List<scalar>\s*', data)
+    if internal and _format(data) == 'binary':
+        endian, _, bits = _arch(data)
+        _, tail = _binary_list(data[internal.end():], 'f' if bits == 32 else 'd', endian)
+    else:
+        tail = data
+    anchor = re.search(rb'\bboundaryField\s*\{', tail)
+    if anchor is None:
+        raise ValueError('boundaryField absent')
+    tail = tail[anchor.end():]
+    # Replace length-delimited binary lists before parsing braces. Binary bytes
+    # may themselves contain braces, newlines or apparent dictionary keywords.
+    arrays = {}
+    if _format(data) == 'binary':
+        endian, _, bits = _arch(data)
+        parts = []
+        while (match := re.search(rb'nonuniform\s+List<scalar>\s*', tail)) is not None:
+            values, rest = _binary_list(tail[match.end():], 'f' if bits == 32 else 'd', endian)
+            key = f'__array_{len(arrays)}'
+            arrays[key] = values
+            parts.append(tail[:match.start()] + key.encode())
+            tail = rest
+        tail = b''.join(parts) + tail
+    text = tail.decode('ascii')
+    blocks = dict(re.findall(r'([\w]+)\s*\{([^{}]*)\}', text))
+    block = blocks.get(patch)
+    if block is None:
+        raise ValueError(f'patch {patch} has no explicit dictionary')
+    bc = re.search(r'\btype\s+(\w+)\s*;', block)
+    uniform = re.search(r'\bvalue\s+uniform\s+([-+0-9.eE]+)\s*;', block)
+    stored = re.search(r'\bvalue\s+(__array_\d+)\s*;', block)
+    listed = re.search(r'\bvalue\s+nonuniform\s+List<scalar>\s+(\d+)\s*\(([^()]*)\)\s*;', block)
+    if uniform:
+        values, method = [float(uniform[1])] * len(owners), 'stored_boundary_value'
+    elif stored:
+        values, method = arrays[stored[1]], 'stored_boundary_value'
+    elif listed:
+        values, method = [float(x) for x in listed[2].split()], 'stored_boundary_value'
+        if len(values) != int(listed[1]):
+            raise ValueError('boundary list length mismatch')
+    elif bc and bc[1] == 'zeroGradient' and path.name.removesuffix('.gz') == 'p':
+        internal_values = read_scalar_field(path)
+        if re.search(rb'internalField\s+uniform\s+', data):
+            values = internal_values * len(owners)
+        else:
+            values = [internal_values[i] for i in owners]
+        method = 'zeroGradient_exact_owner_value'
+    else:
+        raise ValueError(f'{patch}: unsupported boundary without stored values')
+    if len(values) != len(owners) or not all(math.isfinite(x) for x in values):
+        raise ValueError('boundary value count/nonfinite mismatch')
+    return values, method
+
+
+def dimensions(path: Path) -> str | None:
+    match = re.search(rb'\bdimensions\s*\[([^]]+)\]', _bytes(path)[:4096])
+    return ' '.join(match[1].decode('ascii').split()) if match else None
+
+
+def pump_measurements(case: Path) -> tuple[dict, dict, list[str]]:
+    """All retained positive times, with signed inlet phi and boundary p.
+
+    Only the unique inlet/outlet names (case insensitive) are recognized. No
+    reference times or values enter extraction; time alignment is comparator work.
+    """
+    values, evidence, errors = {}, {}, []
+    try:
+        if not static_mesh(case):
+            raise ValueError('pump retained-field fallback requires a static mesh')
+        points, faces, owner, _, paths = mesh_arrays(case)
+        _, vectors, _, _ = planar_face_geometry(points, faces)
+        areas = np.linalg.norm(vectors, axis=1)
+        specs = boundary_specs(case)
+        names = {}
+        for role in ('inlet', 'outlet'):
+            matches = [name for name in specs if name.lower() == role]
+            if len(matches) != 1:
+                raise ValueError(f'ambiguous or absent {role} patch')
+            names[role] = matches[0]
+        slices = {role: slice(specs[name][0], sum(specs[name])) for role, name in names.items()}
+        if any(sl.stop > len(owner) or sl.start == sl.stop for sl in slices.values()):
+            raise ValueError('invalid inlet/outlet face range')
+    except (OSError, ValueError, RuntimeError) as exc:
+        return {}, {}, [str(exc)]
+    histories = {'mass_flow_rate': [], 'pressure_rise': []}
+    phi_dimension: str | None = None
+    refs = {key: set() for key in histories}
+    boundary = foam_path(case / 'constant/polyMesh', 'boundary')
+    mesh_refs = [str(p.relative_to(case)) for p in [*paths, boundary] if p]
+    for directory in sorted((p for p in case.iterdir() if p.is_dir() and _is_time(p.name) and float(p.name) > 0), key=lambda p: float(p.name)):
+        for metric, field in (('mass_flow_rate', 'phi'), ('pressure_rise', 'p')):
+            path = foam_path(directory, field)
+            if path is None:
+                continue
+            try:
+                actual_dimensions = dimensions(path)
+                allowed_dimensions = (
+                    {'1 0 -1 0 0 0 0', '0 3 -1 0 0 0 0'} if field == 'phi'
+                    else {'1 -1 -2 0 0 0 0', '0 2 -2 0 0 0 0'}
+                )
+                if actual_dimensions not in allowed_dimensions:
+                    raise ValueError('unsupported physical dimensions')
+                if field == 'phi':
+                    phi_dimension = actual_dimensions
+                inlet, _ = scalar_boundary(path, names['inlet'], owner[slices['inlet']].tolist())
+                if field == 'phi':
+                    value = math.fsum(inlet)
+                else:
+                    outlet, _ = scalar_boundary(path, names['outlet'], owner[slices['outlet']].tolist())
+                    value = float(np.average(outlet, weights=areas[slices['outlet']]) - np.average(inlet, weights=areas[slices['inlet']]))
+                histories[metric].append({'time': float(directory.name), 'value': value})
+                refs[metric].add(str(path.relative_to(case)))
+            except (OSError, ValueError, RuntimeError, IndexError) as exc:
+                errors.append(f'{directory.name}/{field}: {exc}')
+    for metric, history in histories.items():
+        if history:
+            values[metric] = {'kind': 'time_history', 'quantity': (
+                'explicit_mass_flow' if phi_dimension == '1 0 -1 0 0 0 0' else 'explicit_volumetric_flow'
+            ) if metric == 'mass_flow_rate' else 'pressure_rise', 'points': history}
+            if metric == 'mass_flow_rate':
+                    values[metric]['field_dimensions'] = phi_dimension
+            else:
+                values[metric].update(definition='outlet_minus_inlet_patch_average', source_patches=names)
+            evidence[metric] = sorted(refs[metric] | set(mesh_refs))
+    return values, evidence, errors
diff --git a/benchmarks/evaluation/schema.py b/benchmarks/evaluation/schema.py
new file mode 100644
index 0000000000000000000000000000000000000000..8fd7035d15fb50154f23981226cab5eb79fc1ab9
--- /dev/null
+++ b/benchmarks/evaluation/schema.py
@@ -0,0 +1,21 @@
+from __future__ import annotations
+
+from pathlib import Path
+from typing import Any
+
+from jsonschema import Draft202012Validator, FormatChecker
+
+from .io import read_object
+
+
+SCHEMA_ROOT = Path(__file__).resolve().parents[2] / "schemas"
+
+
+def validate(value: Any, schema_name: str) -> None:
+    schema = read_object(SCHEMA_ROOT / schema_name)
+    validator = Draft202012Validator(schema, format_checker=FormatChecker())
+    errors = sorted(validator.iter_errors(value), key=lambda error: list(error.absolute_path))
+    if errors:
+        error = errors[0]
+        location = ".".join(str(item) for item in error.absolute_path) or "<root>"
+        raise ValueError(f"{schema_name} validation failed at {location}: {error.message}")
diff --git a/benchmarks/evaluation/stability.py b/benchmarks/evaluation/stability.py
new file mode 100644
index 0000000000000000000000000000000000000000..f13cf722d02917b58a53b8e1d2369d7b57b62623
--- /dev/null
+++ b/benchmarks/evaluation/stability.py
@@ -0,0 +1,48 @@
+from __future__ import annotations
+
+import math
+import re
+from pathlib import Path
+from typing import Any
+
+from .foam_io import read_text
+
+
+def numerical_scheme(case_dir: Path) -> str:
+    block = re.search(r"ddtSchemes\s*\{(?P<body>.*?)\}", read_text(case_dir / "system/fvSchemes"), re.S)
+    default = re.search(r"\bdefault\s+([^;\s]+)", block.group("body")) if block else None
+    return default.group(1) if default else "unknown"
+
+
+def steady_plateau(
+    qois: dict[str, Any],
+    baseline_spans: dict[str, float] | None = None,
+    *,
+    final_window_fraction: float = 0.2,
+    minimum_snapshots: int = 3,
+) -> dict[str, Any]:
+    metrics = {}
+    passed = True
+    for name, value in sorted(qois.items()):
+        if not isinstance(value, dict) or value.get("kind") != "time_history":
+            continue
+        points = value.get("points", [])
+        samples = [float(point["value"]) for point in points if isinstance(point, dict)
+                   and isinstance(point.get("value"), (int, float))]
+        if len(samples) < minimum_snapshots:
+            metrics[name] = {"status": "fail", "sample_count": len(samples), "expected_minimum": minimum_snapshots}
+            passed = False
+            continue
+        count = max(minimum_snapshots, math.ceil(len(samples) * final_window_fraction))
+        selected = samples[-count:]
+        span = (max(selected) - min(selected)) / max(abs(selected[-1]), 1e-12)
+        limit = max(0.02, (baseline_spans or {}).get(name, 0.0) * 2.0)
+        ok = span <= limit
+        metrics[name] = {"status": "pass" if ok else "fail", "relative_span": span,
+                         "limit": limit, "sample_count": count}
+        passed = passed and ok
+    return {
+        "status": "pass" if metrics and passed else "fail" if metrics else "not_applicable",
+        "applicable": bool(metrics),
+        "metrics": metrics,
+    }
diff --git a/benchmarks/reference_statistics/advanced.json b/benchmarks/reference_statistics/advanced.json
new file mode 100644
index 0000000000000000000000000000000000000000..c73c76233a0181e39d72fef33f28e22992c80330
--- /dev/null
+++ b/benchmarks/reference_statistics/advanced.json
@@ -0,0 +1,754 @@
+{
+  "schema_version": "easyfoam.reference_statistics.v1",
+  "parser_contract": {
+    "final_window_fraction": 0.2,
+    "minimum_final_window_samples": 5,
+    "final_linear_residual": {
+      "reference_factor": 10.0,
+      "absolute_floor": 0.001
+    },
+    "initial_residual": {
+      "reference_factor": 10.0,
+      "absolute_floor": 0.001
+    },
+    "courant_final_p95": {
+      "reference_factor": 3.0,
+      "absolute_floor": 1.0
+    },
+    "courant_peak": {
+      "reference_factor": 3.0,
+      "absolute_floor": 2.0
+    },
+    "continuity_global_p95": {
+      "reference_factor": 10.0,
+      "absolute_floor": 1e-05
+    },
+    "continuity_cumulative_final": {
+      "reference_factor": 10.0,
+      "absolute_floor": 0.001
+    }
+  },
+  "notes": "Exact numeric outputs of the existing parser; empty objects preserve unavailable source reference diagnostics.",
+  "cases": {
+    "Cavity_LES": {
+      "log_paths": [
+        "reference/advanced/Cavity_LES/log.blockMesh",
+        "reference/advanced/Cavity_LES/log.foamRun"
+      ],
+      "fatal_marker": false,
+      "nonfinite_marker": false,
+      "residual_field_count": 4,
+      "residual_record_count": 10000,
+      "residuals": {
+        "Ux": {
+          "sample_count": 2000,
+          "initial_final_window_p95": 9.711211045e-05,
+          "final_final_window_p95": 3.26750965e-07
+        },
+        "Uy": {
+          "sample_count": 2000,
+          "initial_final_window_p95": 9.454523474999998e-05,
+          "final_final_window_p95": 2.3178064999999995e-07
+        },
+        "k": {
+          "sample_count": 2000,
+          "initial_final_window_p95": 0.000158224749,
+          "final_final_window_p95": 5.9913584e-07
+        },
+        "p": {
+          "sample_count": 4000,
+          "initial_final_window_p95": 0.0001477765745,
+          "final_final_window_p95": 1.417127335e-06
+        }
+      },
+      "initial_residual_final_window_p95": 0.000158224749,
+      "final_residual_final_window_p95": 1.417127335e-06,
+      "courant_count": 2001,
+      "courant_peak": 0.32094299,
+      "courant_final_window_p95": 0.32037435,
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+      "continuity_global_final_window_p95": 7.377479164999997e-19,
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diff --git a/benchmarks/reference_statistics/basic.json b/benchmarks/reference_statistics/basic.json
new file mode 100644
index 0000000000000000000000000000000000000000..9b90e7a6bb2616c2f3b43d20375b15e80a63527a
--- /dev/null
+++ b/benchmarks/reference_statistics/basic.json
@@ -0,0 +1,4494 @@
+{
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diff --git a/benchmarks/reference_statistics/extended.json b/benchmarks/reference_statistics/extended.json
new file mode 100644
index 0000000000000000000000000000000000000000..5eedb03a195553655d9de276e8bf8fea5f84a460
--- /dev/null
+++ b/benchmarks/reference_statistics/extended.json
@@ -0,0 +1,4373 @@
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+}
diff --git a/benchmarks/scripts/__init__.py b/benchmarks/scripts/__init__.py
new file mode 100644
index 0000000000000000000000000000000000000000..5b359f5f10e930be2cc01cbbbaa6edeb85ec4b77
--- /dev/null
+++ b/benchmarks/scripts/__init__.py
@@ -0,0 +1 @@
+"""Reusable benchmark algorithms and their command-line compatibility entry points."""
diff --git a/benchmarks/scripts/build_extbench_reference.py b/benchmarks/scripts/build_extbench_reference.py
new file mode 100644
index 0000000000000000000000000000000000000000..a12472dc0f804d495c347ae3b7d5acf8188bacb8
--- /dev/null
+++ b/benchmarks/scripts/build_extbench_reference.py
@@ -0,0 +1,146 @@
+#!/usr/bin/env python3
+"""Build the executable Extended reference contract from an extraction audit."""
+from __future__ import annotations
+
+import argparse
+import json
+import math
+from pathlib import Path
+from typing import Any
+
+
+STRICTLY_POSITIVE_SCALARS = {"first_cell_yplus", "rise_velocity", "equivalent_radius_final", "final_component_count"}
+NONNEGATIVE_SCALARS = {"spalding_log_rmse", "Cd_rms", "interior_pressure_span"}
+STRICTLY_POSITIVE_STRUCTURED = {
+    "branchwise_wall_law_metrics", "jet_to_mainstream_mass_flux_ratio",
+    "minimum_observed_equivalent_radius", "rise_velocity",
+}
+
+
+def physical_bounds(name: str, *, structured: bool = False) -> dict[str, Any]:
+    if name in STRICTLY_POSITIVE_SCALARS or (structured and name in STRICTLY_POSITIVE_STRUCTURED):
+        return {"physical_low": 1e-12, "physical_threshold_source": "task_implied_positive_response"}
+    if name in NONNEGATIVE_SCALARS:
+        return {"physical_low": 0.0, "physical_threshold_source": "definition_implied_nonnegative_response"}
+    return {}
+
+
+def scalar_tolerance(name: str, value: float) -> dict[str, Any]:
+    # Component counts are discrete physical topology, not a continuously
+    # varying response.  An exact interval prevents a one-component result
+    # from being accepted as a two-component result.
+    discrete = name == "final_component_count"
+    relative = 0.0 if discrete else (0.05 if name in {"Cd", "Cl", "Cm", "Cd_mean"} else 0.10)
+    floor = {
+        "Cd": 5e-4, "Cl": 1e-3, "Cm": 5e-4, "Cd_mean": 5e-4,
+        "Cd_rms": 5e-4, "spalding_log_rmse": 0.05, "first_cell_yplus": 0.05,
+        "interior_pressure_span": 1e-6,
+    }.get(name, max(abs(value) * 1e-6, 1e-12))
+    width = 0.0 if discrete else max(abs(value) * relative, floor)
+    return {
+        "kind": "steady_scalar",
+        "low": value - width,
+        "high": value + width,
+        "relative_component": relative,
+        "absolute_floor": floor,
+        "criterion_role": "principal_response",
+        "reference_independent": False,
+        "threshold_source": "reference_anchored_repeatability_pending",
+        "provisional": True,
+        **physical_bounds(name),
+    }
+
+
+def structured_tolerance(name: str, value: dict[str, Any]) -> dict[str, Any]:
+    kind = value.get("kind")
+    if kind in {"time_history", "component_trajectory", "branched_time_histories"}:
+        return {"kind": "trajectory", "normalized_rmse_max": 0.10, "normalized_linf_max": 0.25,
+                "minimum_time_coverage": 0.90, "normalization_floor": 1e-12,
+                "criterion_role": "principal_response_shape", "reference_independent": False,
+                "threshold_source": "reference_anchored_trajectory", "provisional": True}
+    if kind == "named_profiles":
+        return {"kind": "profile", "normalized_l1_max": 0.08, "normalized_linf_max": 0.20,
+                "normalization_floor": 1e-12, "criterion_role": "principal_response_shape",
+                "reference_independent": False,
+                "threshold_source": "reference_anchored_spatial_response_shape", "provisional": True}
+    if kind == "profile_feature_locations":
+        return {"kind": "event_location", "maximum_cell_offset": 2.0,
+                "physical_floor": 1e-12, "criterion_role": "principal_response_shape",
+                "reference_independent": False,
+                "threshold_source": "reference_anchored_feature_location", "provisional": True}
+    if kind in {"component_scalars", "branch_scalars", "scalar_ratio", "window_regression"}:
+        return {
+            "kind": kind,
+            "relative_max": 0.10,
+            "absolute_floor": 1e-12,
+            "criterion_role": "principal_response",
+            "reference_independent": False,
+            "threshold_source": "reference_anchored_structured_response",
+            "provisional": True,
+            **physical_bounds(name, structured=True),
+        }
+    raise ValueError(f"unsupported reference QoI kind: {kind!r}")
+
+
+def build_reference(audit: dict[str, Any]) -> dict[str, Any]:
+    cases: dict[str, Any] = {}
+    for case_id, record in sorted(audit["cases"].items()):
+        if record.get("status") != "complete":
+            raise ValueError(f"cannot freeze incomplete reference case: {case_id}")
+        qois = record.get("qois", {})
+        tolerances = {}
+        for name, value in qois.items():
+            if isinstance(value, bool):
+                raise ValueError(f"invalid boolean QoI: {case_id}/{name}")
+            if isinstance(value, (int, float)):
+                if not math.isfinite(float(value)):
+                    raise ValueError(f"non-finite QoI: {case_id}/{name}")
+                tolerances[name] = scalar_tolerance(name, float(value))
+            elif isinstance(value, dict):
+                tolerances[name] = structured_tolerance(name, value)
+            else:
+                raise ValueError(f"unsupported QoI: {case_id}/{name}")
+        cases[case_id] = {
+            "case_id": case_id,
+            "family": record.get("family"),
+            "branch_id": record.get("branch_id"),
+            "principal_qoi_group": record.get("branch_id") or record.get("family") or "principal",
+            "principal_metrics": list(record.get("required_metrics", [])),
+            "metric_roles": {name: "principal" for name in qois},
+            "qois": qois,
+            "conditional_metrics": list(record.get("conditional_metrics", [])),
+            "conditional_qois": dict(record.get("conditional_qois", {})),
+            "conditional_status": dict(record.get("conditional_status", {})),
+            "diagnostic_qois": dict(record.get("diagnostic_qois", {})),
+            "tolerances": tolerances,
+            "provenance": {"case_dir": record.get("case_dir"), "evidence": record.get("evidence"),
+                           "metric_methods": record.get("metric_methods")},
+        }
+    return {
+        "schema_version": "foambench.reference_qois",
+        "design": "foambench.qoi.design",
+        "tolerance_status": "joint_physical_admissibility_and_reference_response_provisional",
+        "notes": [
+            "Principal reference bands test task-response agreement and are explicitly reference-anchored.",
+            "Definition-implied physical bounds are evaluated jointly when a sign or positivity rule is unambiguous.",
+            "Conditional QoIs remain unavailable rather than silently passing when their declared evidence is absent.",
+        ],
+        "case_count": len(cases),
+        "cases": cases,
+    }
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--audit", required=True, type=Path)
+    parser.add_argument("--output", required=True, type=Path)
+    args = parser.parse_args()
+    audit = json.loads(args.audit.read_text(encoding="utf-8"))
+    output = build_reference(audit)
+    args.output.parent.mkdir(parents=True, exist_ok=True)
+    args.output.write_text(json.dumps(output, indent=2, sort_keys=True) + "\n", encoding="utf-8")
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/scripts/compare_foambench_qois.py b/benchmarks/scripts/compare_foambench_qois.py
new file mode 100644
index 0000000000000000000000000000000000000000..e97a87392b8441a8877c38fde0bbff49f12eab00
--- /dev/null
+++ b/benchmarks/scripts/compare_foambench_qois.py
@@ -0,0 +1,17 @@
+#!/usr/bin/env python3
+"""Compatibility CLI for the canonical FoamBench QoI comparator."""
+from __future__ import annotations
+
+import sys
+from pathlib import Path
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.comparison import *  # noqa: F401,F403
+from benchmarks.evaluation.comparison import main
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/scripts/extract_extbench_qois.py b/benchmarks/scripts/extract_extbench_qois.py
new file mode 100644
index 0000000000000000000000000000000000000000..c95bcd6aee4e2efd4651da7f84f29b5f62c1d2c5
--- /dev/null
+++ b/benchmarks/scripts/extract_extbench_qois.py
@@ -0,0 +1,17 @@
+#!/usr/bin/env python3
+"""Compatibility CLI for the Extended FoamBench QoI audit extractor."""
+from __future__ import annotations
+
+import sys
+from pathlib import Path
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.extbench import *  # noqa: F401,F403
+from benchmarks.evaluation.extbench import main
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/scripts/extract_foambench_candidate_qois.py b/benchmarks/scripts/extract_foambench_candidate_qois.py
new file mode 100644
index 0000000000000000000000000000000000000000..494db6fa2393315633cbbcd19eb5bec29851d3ae
--- /dev/null
+++ b/benchmarks/scripts/extract_foambench_candidate_qois.py
@@ -0,0 +1,51 @@
+#!/usr/bin/env python3
+"""Compatibility entry point for FoamBench candidate QoI extraction.
+
+Basic and advanced contracts use structured field histories and spatial
+profiles.  Those metrics are implemented by :mod:`basic_advanced`, whereas
+the historical ``field_extractor`` only produces generic scalar diagnostics.
+Keep the latter available for legacy callers, but route contract-backed
+FoamBench cases to the structured implementation.
+"""
+from __future__ import annotations
+
+import sys
+from pathlib import Path
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.field_extractor import *  # noqa: F401,F403
+from benchmarks.evaluation.field_extractor import (
+    extract_case_qois as _legacy_extract_case_qois,
+    required_metrics as _legacy_required_metrics,
+)
+from benchmarks.evaluation.basic_advanced import ADVANCED_TEMPLATE, GROUPS, extract as _structured_extract
+
+
+def _supports_structured_contract(case_id: str) -> bool:
+    """Return whether ``case_id`` belongs to Basic or Advanced FoamBench."""
+    return case_id in ADVANCED_TEMPLATE or case_id.split("/", 1)[0] in GROUPS
+
+
+def extract_case_qois(case_dir, case_id, reference_path=None, log_paths=None):
+    """Extract contract QoIs, preserving the legacy generic fallback.
+
+    Evolution evaluation always provides ``reference_path``.  Its metric set
+    is therefore the authoritative requested/required set for the structured
+    extractor.  Legacy synthetic contracts retain their original behavior.
+    """
+    if reference_path is not None and _supports_structured_contract(case_id):
+        required, _ = _legacy_required_metrics(reference_path, case_id)
+        return _structured_extract(
+            case_dir,
+            case_id,
+            requested_metrics=required,
+            required_metrics=required,
+        )
+    return _legacy_extract_case_qois(case_dir, case_id, reference_path, log_paths)
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/scripts/extract_foambench_qois.py b/benchmarks/scripts/extract_foambench_qois.py
new file mode 100644
index 0000000000000000000000000000000000000000..5c742492c19fedf088b04238bdd697f56040ab1f
--- /dev/null
+++ b/benchmarks/scripts/extract_foambench_qois.py
@@ -0,0 +1,17 @@
+#!/usr/bin/env python3
+"""Compatibility CLI for the canonical FoamBench reference extractor."""
+from __future__ import annotations
+
+import sys
+from pathlib import Path
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.qoi_reference import *  # noqa: F401,F403
+from benchmarks.evaluation.qoi_reference import main
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/benchmarks/scripts/materialize_benchmark.py b/benchmarks/scripts/materialize_benchmark.py
new file mode 100644
index 0000000000000000000000000000000000000000..bc743308963db7704a59153707737629e465a1ca
--- /dev/null
+++ b/benchmarks/scripts/materialize_benchmark.py
@@ -0,0 +1,240 @@
+#!/usr/bin/env python3
+"""Materialize OpenFOAM cases from a FoamBench JSON export.
+
+The Basic benchmark uses ``family/variant`` identifiers while Advanced uses
+single-component identifiers. This script deliberately keeps either
+representation lossless: it only creates the case tree and a manifest; it
+does not edit controlDict files or shorten the requested simulation.
+"""
+from __future__ import annotations
+
+import argparse
+import hashlib
+import json
+import os
+import re
+import shutil
+import sys
+from pathlib import Path
+from typing import Any
+
+
+CASE_KEY = re.compile(r"^[^/\\]+(?:/[^/\\]+)?$")
+COMMAND_MARKERS = (
+    "decomposePar",
+    "runParallel",
+    "reconstructPar",
+    "topoSet",
+    "setFields",
+    "checkMesh",
+    "createPatch",
+    "blockMesh",
+    "foamRun",
+    "foamPostProcess",
+)
+
+
+def sha256_bytes(data: bytes) -> str:
+    return hashlib.sha256(data).hexdigest()
+
+
+def sha256_file(path: Path) -> str:
+    digest = hashlib.sha256()
+    with path.open("rb") as stream:
+        for chunk in iter(lambda: stream.read(1024 * 1024), b""):
+            digest.update(chunk)
+    return digest.hexdigest()
+
+
+def tree_sha256(root: Path) -> str:
+    """Hash relative paths and bytes, independent of directory iteration order."""
+    digest = hashlib.sha256()
+    for path in sorted(p for p in root.rglob("*") if p.is_file()):
+        relative = path.relative_to(root).as_posix().encode("utf-8")
+        digest.update(len(relative).to_bytes(8, "big"))
+        digest.update(relative)
+        digest.update(bytes.fromhex(sha256_file(path)))
+    return digest.hexdigest()
+
+
+def safe_relative_key(key: str) -> Path:
+    path = Path(key)
+    if path.is_absolute() or key.startswith(("/", "\\")):
+        raise ValueError(f"absolute case key is not allowed: {key!r}")
+    if any(part in ("", ".", "..") for part in path.parts):
+        raise ValueError(f"unsafe case key: {key!r}")
+    if len(path.parts) < 1:
+        raise ValueError(f"empty case key: {key!r}")
+    return path
+
+
+def variant_sort_key(case_id: str) -> tuple[Any, ...]:
+    family, variant = case_id.split("/", 1) if "/" in case_id else (case_id, "default")
+    chunks = re.split(r"(\d+)", variant)
+    normalized: list[Any] = []
+    for chunk in chunks:
+        normalized.append((0, int(chunk)) if chunk.isdigit() else (1, chunk))
+    return (family, normalized)
+
+
+def choose_case_ids(data: dict[str, Any], requested: list[str] | None, excluded: set[str] | None = None) -> list[str]:
+    excluded = excluded or set()
+    if requested:
+        unknown = sorted(set(requested) - set(data))
+        if unknown:
+            raise ValueError("case id(s) not found: " + ", ".join(unknown))
+        return requested
+    families: dict[str, list[str]] = {}
+    for case_id in data:
+        if not CASE_KEY.match(case_id):
+            raise ValueError(f"unsafe case id: {case_id!r}")
+        family = case_id.split("/", 1)[0] if "/" in case_id else case_id
+        families.setdefault(family, []).append(case_id)
+    return [sorted(ids, key=variant_sort_key)[0] for _, ids in sorted(families.items()) if ids and sorted(ids, key=variant_sort_key)[0] not in excluded]
+
+
+def materialize_assets(case_id: str, spec: dict[str, Any], case_root: Path | None,
+                       source: Path, asset_manifest: dict[str, Any] | None = None) -> list[dict[str, str]]:
+    """Verify declared geometry and optionally copy it, without reference case files."""
+    records = []
+    if spec.get("_external_assets"):
+        if asset_manifest is None:
+            raise ValueError(f"{case_id}: external assets declared but no asset manifest was found")
+        entries = asset_manifest.get("assets", {})
+        for asset in spec["_external_assets"]:
+            if not isinstance(asset, dict) or not isinstance(asset.get("asset_id"), str) or not isinstance(asset.get("target"), str):
+                raise ValueError(f"{case_id}: malformed external asset declaration")
+            asset_id = asset["asset_id"]
+            record = entries.get(asset_id)
+            if not isinstance(record, dict):
+                raise ValueError(f"{case_id}: unknown asset_id {asset_id!r}")
+            asset_path = Path(record.get("path", ""))
+            if asset_path.is_absolute() or ".." in asset_path.parts:
+                raise ValueError(f"{case_id}: unsafe asset path for {asset_id!r}")
+            asset_file = source.parent.parent / asset_path
+            if not asset_file.is_file():
+                raise ValueError(f"{case_id}: asset file does not exist: {asset_file}")
+            expected = record.get("sha256")
+            if not isinstance(expected, str) or sha256_file(asset_file) != expected:
+                raise ValueError(f"{case_id}: SHA-256 mismatch for asset {asset_id!r}")
+            relative = safe_relative_key(asset["target"])
+            records.append({"asset_id": asset_id, "target": relative.as_posix(), "sha256": expected})
+            if case_root is not None:
+                target = case_root / relative
+                if not target.resolve().is_relative_to(case_root.resolve()):
+                    raise ValueError(f"{case_id}: asset target escapes case root")
+                target.parent.mkdir(parents=True, exist_ok=True)
+                shutil.copyfile(asset_file, target)
+    return records
+
+
+def materialize_case(case_id: str, spec: dict[str, Any], case_root: Path, source: Path, asset_manifest: dict[str, Any] | None = None) -> dict[str, Any]:
+    case_root.mkdir(parents=True, exist_ok=False)
+    allrun = spec.get("Allrun")
+    blocked = not isinstance(allrun, str)
+    if blocked:
+        allrun = ""
+    materialize_assets(case_id, spec, case_root, source, asset_manifest)
+    for key, content in spec.items():
+        if key == "usr_requirement" or key.startswith("_") or key == "reference_subcases":
+            continue
+        relative = safe_relative_key(key)
+        if not isinstance(content, str):
+            raise ValueError(f"{case_id}: file content for {key!r} is not text")
+        target = case_root / relative
+        target.parent.mkdir(parents=True, exist_ok=True)
+        target.write_text(content, encoding="utf-8", newline="")
+        if key == "Allrun":
+            target.chmod(target.stat().st_mode | 0o111)
+    if blocked:
+        (case_root / "BLOCKED_REFERENCE.txt").write_text(
+            "This task has no runnable reference case. See the repair status report.\n"
+            + str(spec.get("usr_requirement", "")) + "\n",
+            encoding="utf-8",
+        )
+    operations = [marker for marker in COMMAND_MARKERS if re.search(rf"\b{re.escape(marker)}\b", allrun)]
+    family, variant = case_id.split("/", 1) if "/" in case_id else (case_id, "default")
+    return {
+        "case_id": case_id,
+        "family": family,
+        "variant": variant,
+        "source_json": str(source.resolve()),
+        "source_json_sha256": sha256_file(source),
+        "usr_requirement": spec.get("usr_requirement", ""),
+        "allrun": allrun,
+        "workflow_operations": operations,
+        "case_sha256": tree_sha256(case_root),
+        "file_count": sum(1 for p in case_root.rglob("*") if p.is_file()),
+    }
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--benchmark", type=Path, required=True)
+    parser.add_argument("--output-root", type=Path, required=True)
+    parser.add_argument("--case-id", action="append", help="select a case; repeat to select several")
+    parser.add_argument("--status", type=Path, help="repair status JSON; blocked cases are excluded from default selection")
+    parser.add_argument("--asset-manifest", type=Path, help="asset manifest; defaults to benchmarks/assets/manifest.json next to the benchmark")
+    parser.add_argument("--allow-existing", action="store_true", help="allow an existing empty output root")
+    args = parser.parse_args()
+
+    source = args.benchmark.resolve(strict=True)
+    output = args.output_root.resolve()
+    data = json.loads(source.read_text(encoding="utf-8"))
+    if not isinstance(data, dict):
+        raise ValueError("benchmark JSON root must be an object")
+    asset_manifest_path = args.asset_manifest.resolve() if args.asset_manifest else source.parent / "assets" / "manifest.json"
+    asset_manifest = None
+    if asset_manifest_path.exists():
+        asset_manifest = json.loads(asset_manifest_path.read_text(encoding="utf-8"))
+    status_path = args.status
+    if status_path is None:
+        candidates = [
+            source.with_name(source.name.replace("_repaired.json", "_repair_status.json")),
+            source.with_name(source.name.replace(".json", "_repair_status.json")),
+        ]
+        status_path = next((candidate for candidate in candidates if candidate.exists()), None)
+    excluded: set[str] = set()
+    if status_path and status_path.exists() and not args.case_id:
+        status_data = json.loads(status_path.read_text(encoding="utf-8"))
+        excluded = set(status_data.get("excluded_from_default_scientific_denominator", []))
+    case_ids = choose_case_ids(data, args.case_id, excluded)
+    if output.exists():
+        existing = list(output.iterdir())
+        if existing and not args.allow_existing:
+            raise ValueError(f"output root is not empty: {output}; choose a new path or --allow-existing")
+    output.mkdir(parents=True, exist_ok=True)
+    track = output.name
+    cases: list[dict[str, Any]] = []
+    for case_id in case_ids:
+        safe_name = case_id.replace("/", "__")
+        case_dir = output / safe_name / "case"
+        if case_dir.parent.exists():
+            raise ValueError(f"case output already exists: {case_dir.parent}")
+        metadata = materialize_case(case_id, data[case_id], case_dir, source, asset_manifest)
+        metadata["track"] = track
+        metadata_path = case_dir.parent / "metadata.json"
+        metadata_path.write_text(json.dumps(metadata, ensure_ascii=False, indent=2) + "\n", encoding="utf-8")
+        cases.append({"case_id": case_id, "relative_dir": safe_name, **metadata})
+    manifest = {
+        "schema_version": "m0.materialized.v1",
+        "track": track,
+        "benchmark": str(source),
+        "benchmark_sha256": sha256_file(source),
+        "selection": "first_sorted_variant_per_family" if not args.case_id else "explicit_case_ids",
+        "case_count": len(cases),
+        "cases": cases,
+    }
+    (output / "manifest.json").write_text(json.dumps(manifest, ensure_ascii=False, indent=2) + "\n", encoding="utf-8")
+    print(f"materialized {len(cases)} cases into {output}")
+    for item in cases:
+        print(f"  {item['track']}: {item['case_id']} ({','.join(item['workflow_operations']) or 'no detected operations'})")
+    return 0
+
+
+if __name__ == "__main__":
+    try:
+        raise SystemExit(main())
+    except (OSError, ValueError, json.JSONDecodeError) as exc:
+        print(f"materialize_benchmark.py: error: {exc}", file=sys.stderr)
+        raise SystemExit(2)
diff --git a/benchmarks/scripts/recover_extbench_qoi.py b/benchmarks/scripts/recover_extbench_qoi.py
new file mode 100644
index 0000000000000000000000000000000000000000..55059764f482f7a86687550d367492dabb860da7
--- /dev/null
+++ b/benchmarks/scripts/recover_extbench_qoi.py
@@ -0,0 +1,293 @@
+#!/usr/bin/env python3
+"""Recover incomplete QoI comparisons from frozen Extended FoamBench cases.
+
+The driver never invokes a solver and never edits a source run.  It consumes
+an existing ``campaign_evaluation.json`` and follows each record's explicit
+``artifact.case_dir``.  Only execution-pass cases whose original QoI status
+contains ``incomplete`` are selected.
+"""
+from __future__ import annotations
+
+import argparse
+import json
+import sys
+from collections import defaultdict
+from datetime import datetime, timezone
+from pathlib import Path
+from typing import Any
+
+ROOT = Path(__file__).resolve().parents[2]
+if str(ROOT) not in sys.path:
+    sys.path.insert(0, str(ROOT))
+
+from benchmarks.evaluation.aggregate import aggregate_results
+from benchmarks.evaluation.extbench import extract_contract_case
+from benchmarks.evaluation.frozen_recovery import (
+    RECOVERY_VERSION,
+    document_checksum,
+    recover_case,
+    recovery_score_record,
+)
+from benchmarks.evaluation.comparison import compare_case
+from benchmarks.evaluation.io import write_json
+
+
+DEFAULT_REFERENCE = ROOT / "benchmarks/FoamBench_extended_openfoam13_reference_qois.json"
+DEFAULT_DESIGN = ROOT / "benchmarks/FoamBench_extended_openfoam13_qoi_design.json"
+
+
+def utc_now() -> str:
+    return datetime.now(timezone.utc).isoformat()
+
+
+def load_json(path: Path) -> dict[str, Any]:
+    value = json.loads(path.read_text(encoding="utf-8"))
+    if not isinstance(value, dict):
+        raise ValueError(f"expected an object in {path}")
+    return value
+
+
+def compact_failure_record(
+    source: dict[str, Any],
+    case_id: str,
+    reference: dict[str, Any],
+    design: dict[str, Any],
+    adapter: str,
+    error: Exception,
+) -> dict[str, Any]:
+    """Keep one malformed case auditable without aborting other recoveries."""
+    case_dir = Path(str(source.get("artifact", {}).get("case_dir", "")))
+    candidate: dict[str, Any]
+    try:
+        candidate = extract_contract_case(case_dir, case_id, design)
+        comparison = compare_case(reference, candidate, 1.0)
+    except Exception as nested:
+        candidate = {
+            "schema_version": "foambench.qoi.candidate",
+            "case_id": case_id,
+            "required_metrics": list(reference.get("qois", {})),
+            "missing_metrics": sorted(reference.get("qois", {})),
+            "qois": {},
+            "status": "incomplete",
+            "health": {"status": "incomplete", "reason": str(nested)},
+        }
+        comparison = {
+            "schema_version": "foambench.qoi.case_comparison.v3",
+            "status": "incomplete",
+            "missing_metrics": sorted(reference.get("qois", {})),
+            "out_of_tolerance_metrics": [],
+            "invalid_contract_metrics": [],
+            "physics_grounded_qoi_pass": False,
+            "qoi_pass_ratio": 0.0,
+        }
+    return {
+        "case_id": case_id,
+        "family": case_id.split("/", 1)[0],
+        "variant": case_id.split("/", 1)[1],
+        "case_dir": str(case_dir),
+        "original": {
+            "reextract_status": comparison.get("status"),
+            "reextract_missing_metrics": comparison.get("missing_metrics", []),
+            "reextract_candidate_missing_metrics": candidate.get("missing_metrics", []),
+        },
+        "recovery": {
+            "status": "irrecoverable_incomplete",
+            "version": RECOVERY_VERSION,
+            "methods": {},
+            "source_evidence": {},
+            "source_times": [],
+            "preflight": {"status": "error"},
+            "reasons": [f"recovery driver exception: {error}"],
+        },
+        "candidate": candidate,
+        "comparison": comparison,
+    }
+
+
+def select_case_ids(campaign: dict[str, Any], requested: list[str] | None) -> list[str]:
+    cases = campaign.get("cases")
+    if not isinstance(cases, dict):
+        raise ValueError("campaign has no cases object")
+    selected = sorted(requested or cases)
+    unknown = sorted(set(selected) - set(cases))
+    if unknown:
+        raise ValueError("unknown case IDs: " + ", ".join(unknown))
+    filtered: list[str] = []
+    for case_id in selected:
+        record = cases[case_id]
+        if not isinstance(record, dict):
+            continue
+        execution = record.get("execution", {})
+        qoi = record.get("qoi", {})
+        if execution.get("status") == "pass" and "incomplete" in str(qoi.get("status", "")):
+            filtered.append(case_id)
+    return filtered
+
+
+def family_summary(rows: dict[str, dict[str, Any]]) -> dict[str, Any]:
+    grouped: dict[str, list[dict[str, Any]]] = defaultdict(list)
+    for row in rows.values():
+        grouped[str(row.get("family"))].append(row)
+    result: dict[str, Any] = {}
+    for family, family_rows in sorted(grouped.items()):
+        statuses = [row.get("recovery", {}).get("status") for row in family_rows]
+        result[family] = {
+            "selected_case_count": len(family_rows),
+            "recovered_complete_count": statuses.count("recovered_complete"),
+            "recovered_out_of_tolerance_count": statuses.count("recovered_out_of_tolerance"),
+            "irrecoverable_incomplete_count": statuses.count("irrecoverable_incomplete"),
+            "original_incomplete_count": len(family_rows),
+            "final_incomplete_count": sum("incomplete" in str(row.get("comparison", {}).get("status")) for row in family_rows),
+            "cases": sorted(row["case_id"] for row in family_rows),
+        }
+    return result
+
+
+def run(args: argparse.Namespace) -> int:
+    campaign_path = args.campaign.resolve(strict=True)
+    reference_path = args.reference_qois.resolve(strict=True)
+    design_path = args.design.resolve(strict=True)
+    output = args.output.resolve()
+    campaign = load_json(campaign_path)
+    reference_doc = load_json(reference_path)
+    design = load_json(design_path)
+    references = reference_doc.get("cases")
+    if not isinstance(references, dict):
+        raise ValueError(f"reference document has no cases object: {reference_path}")
+    adapter = args.adapter or str(campaign.get("adapter", ""))
+    if adapter not in {"easyfoam", "foamagent"}:
+        raise ValueError("--adapter must be easyfoam or foamagent")
+    selected = select_case_ids(campaign, args.case_id)
+    if not selected:
+        raise ValueError("no execution-pass incomplete cases selected from campaign")
+    missing_reference = sorted(set(selected) - set(references))
+    if missing_reference:
+        raise ValueError("reference document is missing selected cases: " + ", ".join(missing_reference))
+
+    recovered: dict[str, dict[str, Any]] = {}
+    scored_rows: dict[str, dict[str, Any]] = {}
+    for case_id in selected:
+        source = campaign["cases"][case_id]
+        raw_case_dir = source.get("artifact", {}).get("case_dir")
+        if not isinstance(raw_case_dir, str) or not raw_case_dir:
+            raise ValueError(f"{case_id}: campaign record has no artifact.case_dir")
+        case_dir = Path(raw_case_dir).resolve()
+        if not case_dir.is_dir():
+            raise ValueError(f"{case_id}: artifact case directory does not exist: {case_dir}")
+        try:
+            item = recover_case(case_id, case_dir, references[case_id], adapter=adapter, design=design)
+        except Exception as exc:
+            item = compact_failure_record(source, case_id, references[case_id], design, adapter, exc)
+        source_qoi = source.get("qoi", {}) if isinstance(source.get("qoi"), dict) else {}
+        source_comparison = source_qoi.get("comparison", {}) if isinstance(source_qoi.get("comparison"), dict) else {}
+        source_candidate = source_qoi.get("candidate", {}) if isinstance(source_qoi.get("candidate"), dict) else {}
+        item.setdefault("original", {}).update({
+            "campaign_status": source_qoi.get("status"),
+            "campaign_missing_metrics": source_comparison.get("missing_metrics", []),
+            "campaign_out_of_tolerance_metrics": source_comparison.get("out_of_tolerance_metrics", []),
+            "campaign_candidate_missing_metrics": source_candidate.get("missing_metrics", []),
+        })
+        recovered[case_id] = item
+        scored_rows[case_id] = recovery_score_record(source, item)
+
+    overall = aggregate_results(list(scored_rows.values()))
+    families: dict[str, dict[str, Any]] = {}
+    for family in sorted({row["family"] for row in scored_rows.values()}):
+        families[family] = aggregate_results([row for row in scored_rows.values() if row["family"] == family])
+    recovery_statuses = [item["recovery"]["status"] for item in recovered.values()]
+    comparison_statuses = [item["comparison"].get("status") for item in recovered.values()]
+    summary = {
+        "schema_version": RECOVERY_VERSION,
+        "generated_at": utc_now(),
+        "source_campaign": str(campaign_path),
+        "adapter": adapter,
+        "selected_case_count": len(selected),
+        "original_incomplete_case_count": len(selected),
+        "final_incomplete_case_count": sum("incomplete" in str(status) for status in comparison_statuses),
+        "recovered_complete_count": recovery_statuses.count("recovered_complete"),
+        "recovered_out_of_tolerance_count": recovery_statuses.count("recovered_out_of_tolerance"),
+        "irrecoverable_incomplete_count": recovery_statuses.count("irrecoverable_incomplete"),
+        "comparison_status_counts": {status: comparison_statuses.count(status) for status in sorted(set(comparison_statuses))},
+        "overall": overall,
+        "families": families,
+        "recovery_families": family_summary(recovered),
+    }
+    manifest = {
+        "schema_version": RECOVERY_VERSION,
+        "generated_at": summary["generated_at"],
+        "scope": "frozen execution-pass cases originally classified incomplete",
+        "solver_rerun": False,
+        "source_campaign": document_checksum(campaign_path),
+        "reference_contract": document_checksum(reference_path),
+        "design_contract": document_checksum(design_path),
+        "adapter": adapter,
+        "selected_case_ids": selected,
+        "selection_rule": "execution.status == pass and 'incomplete' in qoi.status",
+        "case_statuses": {case_id: item["recovery"] for case_id, item in recovered.items()},
+    }
+    campaign_recovery = {
+        "schema_version": RECOVERY_VERSION,
+        "generated_at": summary["generated_at"],
+        "dataset": campaign.get("dataset", "extended"),
+        "adapter": adapter,
+        "run_root": campaign.get("run_root"),
+        "source_campaign": str(campaign_path),
+        "reference_qois": str(reference_path),
+        "design_contract": str(design_path),
+        "scope": "selected execution-pass incomplete cases only",
+        "overall": overall,
+        "families": families,
+        "summary": summary,
+        "cases": scored_rows,
+    }
+    candidate_document = {
+        "schema_version": "foambench.qoi.recovered_candidate.v1",
+        "generated_at": summary["generated_at"],
+        "source_campaign": str(campaign_path),
+        "reference_qois": str(reference_path),
+        "cases": {case_id: item["candidate"] for case_id, item in recovered.items()},
+    }
+    comparison_document = {
+        "schema_version": "foambench.qoi.recovered_comparison.v1",
+        "generated_at": summary["generated_at"],
+        "source_campaign": str(campaign_path),
+        "reference_qois": str(reference_path),
+        "cases": {case_id: item["comparison"] for case_id, item in recovered.items()},
+    }
+    output.mkdir(parents=True, exist_ok=True)
+    write_json(output / "campaign_evaluation.json", campaign_recovery)
+    write_json(output / "recovered_candidate_qois.json", candidate_document)
+    write_json(output / "recovered_comparisons.json", comparison_document)
+    write_json(output / "manifest.json", manifest)
+    write_json(output / "summary.json", summary)
+    for case_id, item in recovered.items():
+        family, variant = case_id.split("/", 1)
+        write_json(output / "cases" / family / f"{variant}.json", item)
+    print(
+        f"frozen QoI recovery: {output} "
+        f"selected={len(selected)} final_incomplete={summary['final_incomplete_case_count']} "
+        f"recovered_complete={summary['recovered_complete_count']} "
+        f"recovered_out_of_tolerance={summary['recovered_out_of_tolerance_count']} "
+        f"irrecoverable={summary['irrecoverable_incomplete_count']}"
+    )
+    return 0
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--campaign", required=True, type=Path, help="existing campaign_evaluation.json")
+    parser.add_argument("--reference-qois", type=Path, default=DEFAULT_REFERENCE)
+    parser.add_argument("--design", type=Path, default=DEFAULT_DESIGN)
+    parser.add_argument("--adapter", choices=("easyfoam", "foamagent"))
+    parser.add_argument("--output", required=True, type=Path)
+    parser.add_argument("--case-id", action="append", help="optional repeated case selection")
+    args = parser.parse_args()
+    return run(args)
+
+
+if __name__ == "__main__":
+    try:
+        raise SystemExit(main())
+    except (OSError, ValueError, json.JSONDecodeError) as exc:
+        print(f"recover_extbench_qoi.py: error: {exc}", file=sys.stderr)
+        raise SystemExit(2)
diff --git a/benchmarks/scripts/validate_benchmark_assets.py b/benchmarks/scripts/validate_benchmark_assets.py
new file mode 100644
index 0000000000000000000000000000000000000000..4fa38add9a5e1437c7d0ede457d068ba76dc138a
--- /dev/null
+++ b/benchmarks/scripts/validate_benchmark_assets.py
@@ -0,0 +1,90 @@
+#!/usr/bin/env python3
+"""Validate bundled FoamBench assets and benchmark references."""
+from __future__ import annotations
+
+import argparse
+import hashlib
+import json
+import re
+from pathlib import Path
+from typing import Any
+
+
+LOCAL_PATH = re.compile(r"/(?:opt|data1|home)/")
+
+
+def sha256(path: Path) -> str:
+    digest = hashlib.sha256()
+    with path.open("rb") as stream:
+        for chunk in iter(lambda: stream.read(1024 * 1024), b""):
+            digest.update(chunk)
+    return digest.hexdigest()
+
+
+def iter_strings(value: Any):
+    if isinstance(value, dict):
+        for child in value.values():
+            yield from iter_strings(child)
+    elif isinstance(value, list):
+        for child in value:
+            yield from iter_strings(child)
+    elif isinstance(value, str):
+        yield value
+
+
+def main() -> int:
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument("--benchmark", type=Path, required=True)
+    parser.add_argument("--manifest", type=Path, required=True)
+    args = parser.parse_args()
+
+    benchmark_path = args.benchmark.resolve(strict=True)
+    manifest_path = args.manifest.resolve(strict=True)
+    benchmark = json.loads(benchmark_path.read_text(encoding="utf-8"))
+    manifest = json.loads(manifest_path.read_text(encoding="utf-8"))
+    assets = manifest.get("assets")
+    if not isinstance(benchmark, dict) or not isinstance(assets, dict):
+        raise ValueError("benchmark and asset manifest roots must be objects")
+
+    local_paths = [text for text in iter_strings(benchmark) if LOCAL_PATH.search(text)]
+    if local_paths:
+        raise ValueError(f"benchmark contains {len(local_paths)} machine-local absolute path(s)")
+
+    repo_root = benchmark_path.parent.parent
+    referenced: set[str] = set()
+    case_count = 0
+    reference_count = 0
+    for case_id, case in benchmark.items():
+        declarations = case.get("_external_assets", [])
+        if declarations:
+            case_count += 1
+        for declaration in declarations:
+            asset_id = declaration.get("asset_id")
+            target = Path(declaration.get("target", ""))
+            if not isinstance(asset_id, str) or asset_id not in assets:
+                raise ValueError(f"{case_id}: unknown asset_id {asset_id!r}")
+            if target.is_absolute() or ".." in target.parts:
+                raise ValueError(f"{case_id}: unsafe asset target {str(target)!r}")
+            referenced.add(asset_id)
+            reference_count += 1
+
+    for asset_id, record in assets.items():
+        relative = Path(record.get("path", ""))
+        if relative.is_absolute() or ".." in relative.parts:
+            raise ValueError(f"{asset_id}: unsafe manifest path")
+        path = repo_root / relative
+        if not path.is_file():
+            raise ValueError(f"{asset_id}: missing file {path}")
+        expected = record.get("sha256")
+        if not isinstance(expected, str) or sha256(path) != expected:
+            raise ValueError(f"{asset_id}: SHA-256 mismatch")
+
+    unreferenced = sorted(set(assets) - referenced)
+    if unreferenced:
+        raise ValueError("unreferenced manifest assets: " + ", ".join(unreferenced))
+    print(f"validated {len(assets)} assets, {reference_count} references, and {case_count} cases")
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())
diff --git a/data/advanced.jsonl b/data/advanced.jsonl
new file mode 100644
index 0000000000000000000000000000000000000000..c9823d0b7114a3c4bcaa63589f2869e72ee9ced9
--- /dev/null
+++ b/data/advanced.jsonl
@@ -0,0 +1,16 @@
+{"task_id": "advanced:Cavity_LES", "track": "advanced", "case_id": "Cavity_LES", "family": "Cavity_LES", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible large eddy simulation (using dynamic kinetic energy equation model) of lid driven cavity flow using pisoFoam solver. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Cavity_SA", "track": "advanced", "case_id": "Cavity_SA", "family": "Cavity_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible of lid driven cavity flow using pisoFoam solver and SpalartAllmaras turbulence model. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Cavity_geometry_1", "track": "advanced", "case_id": "Cavity_geometry_1", "family": "Cavity_geometry_1", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible of lid driven cavity flow using pisoFoam solver and SpalartAllmaras turbulence model. The cavity is a square with dimensions normalized to 2 unit on both the x and y axes and very thin in the z-direction (0.1 unit) and scale the domain down by a factor of 0.1. Use a grid of 40X40 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Cylinder_LES", "track": "advanced", "case_id": "Cylinder_LES", "family": "Cylinder_LES", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a offsetcylinder simulation using Large eddy simulation with dynamic kinetic energy equation model. Use PIMPLE algorithm. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Cylinder_SA", "track": "advanced", "case_id": "Cylinder_SA", "family": "Cylinder_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a offsetcylinder simulation using SpalartAllmaras turbulence model. Use PIMPLE algorithm. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Diamond_Obstacle_KOMEGASST", "track": "advanced", "case_id": "Diamond_Obstacle_KOMEGASST", "family": "Diamond_Obstacle_KOMEGASST", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D diamond obstacle using the k-Omega SST RANS turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The diamond obstacle is a square rotated by 45 degrees with diagonal length of 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to diamond. Use sufficient grid points to discretize the domain and dont use more than 10000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The diamond obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Diamond_Obstacle_SA", "track": "advanced", "case_id": "Diamond_Obstacle_SA", "family": "Diamond_Obstacle_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D diamond obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The diamond obstacle is a square rotated by 45 degrees with diagonal length of 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to diamond. Use sufficient grid points to discretize the domain and dont use more than 10000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The diamond obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Double_Square_SA", "track": "advanced", "case_id": "Double_Square_SA", "family": "Double_Square_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform an incompressible turbulent flow simulation over two square obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 5 in x direction and 0 to 2.5 in y direction and -0.5 to 0.5 in z direction. One of the square obstacle is of size  1 unit x 1 unit x 1 unit centered at 1.5 x 1.25 x 0.0 and the other square obstacle is of size 1 unit x 1 unit x 1 unit centered at 3.5 x 1.25 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 5000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Rectangular_Obstacle_KOMEGASST", "track": "advanced", "case_id": "Rectangular_Obstacle_KOMEGASST", "family": "Rectangular_Obstacle_KOMEGASST", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D rectangular obstacle using the k-Omega SST RANS turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The rectangular obstacle is of size  1 unit x 1 unit x 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 60000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:Rectangular_Obstacle_SA", "track": "advanced", "case_id": "Rectangular_Obstacle_SA", "family": "Rectangular_Obstacle_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform an incompressible turbulent flow simulation over a 2D rectangular obstacle using the SpalartAllmaras turbulence model and pimpleFoam solver. The computational domain spans 0 to 15 in x direction and 0 to 5 in y direction and -0.5 to 0.5 in z direction. The rectangular obstacle is of size  1 unit x 1 unit x 1 unit centered at 2.5 x 2.5 x 0.0. Use one cell in z direction making the geometry effectively 2D. Refine the mesh near to rectangle. Use sufficient grid points to discretize the domain and dont use more than 60000 cells in your mesh. The left boundary is the inlet which uses a uniform velocity of (1,0,0) m/s. The right boundary is the outlet using zero gradient pressure condition. Top and bottom boundaries are fixed walls with nop-slip condition. The front and back faces are empty. The rectangular obstacle also has no-slip boundary condition on its surface. The kinematic viscosity is 2e-6 m2/s. Use a deltaT of 0.5 s and run till a final time of 5 s. Write the results at every 0.5 s. Use a maximum courant number of 1.0. Use OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:counterFlowFlame2D_KE", "track": "advanced", "case_id": "counterFlowFlame2D_KE", "family": "counterFlowFlame2D_KE", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM, employing a compressible flow solver for detailed combustion modeling. Use k-epsilon turbulence model. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with foamRun -solver multicomponentFluid, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:counterFlowFlame2D_SA", "track": "advanced", "case_id": "counterFlowFlame2D_SA", "family": "counterFlowFlame2D_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM, employing a compressible flow solver for detailed combustion modeling. Use SpalartAllmaras turbulence model. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with foamRun -solver multicomponentFluid, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:nozzleFlow2D_SA", "track": "advanced", "case_id": "nozzleFlow2D_SA", "family": "nozzleFlow2D_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D nozzle flow simulation using interfoam solver and  Spalart-Allmaras turbulence model. Use a time step of 1e-8 seconds, output results every 1e-06s. The end time is 1e-5s. seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:obliqueShock_KE", "track": "advanced", "case_id": "obliqueShock_KE", "family": "obliqueShock_KE", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use k-epsilon turbulence model. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:obliqueShock_LES", "track": "advanced", "case_id": "obliqueShock_LES", "family": "obliqueShock_LES", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave LES simulation (Smagorinsky model) using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "advanced:wedge_SA", "track": "advanced", "case_id": "wedge_SA", "family": "wedge_SA", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge using. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 5 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The Pr for the mixture is 1. Use rhoCentralFoam solver. Use SpalartAllmaras turbulence model. The wedge surface is a slip boundary. Use OpenFOAM-13 with foamRun -solver shockFluid, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
diff --git a/data/basic.jsonl b/data/basic.jsonl
new file mode 100644
index 0000000000000000000000000000000000000000..8b3f72d0ee95b79736fc5264e136f34ed112ef32
--- /dev/null
+++ b/data/basic.jsonl
@@ -0,0 +1,110 @@
+{"task_id": "basic:BernardCells/1", "track": "basic", "case_id": "BernardCells/1", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t=1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 301 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/10", "track": "basic", "case_id": "BernardCells/10", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/2", "track": "basic", "case_id": "BernardCells/2", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/3", "track": "basic", "case_id": "BernardCells/3", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/4", "track": "basic", "case_id": "BernardCells/4", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 300 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/5", "track": "basic", "case_id": "BernardCells/5", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/6", "track": "basic", "case_id": "BernardCells/6", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 305 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/7", "track": "basic", "case_id": "BernardCells/7", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/8", "track": "basic", "case_id": "BernardCells/8", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 310 K, while the other has a temperature of 290 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:BernardCells/9", "track": "basic", "case_id": "BernardCells/9", "family": "BernardCells", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 3D Bernard Cell simulation using OpenFOAM buoyantFoam solver. The computational domain spans 9 m x 1 m x 2 m. The simulation begins at t=0 seconds and runs until t = 1000 seconds with a time step of 1 second, and results are written at intervals of every 50 seconds. One wall has a temperature of 315 K, while the other has a temperature of 295 K. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy buoyantFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/1", "track": "basic", "case_id": "Cavity/1", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1 m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/10", "track": "basic", "case_id": "Cavity/10", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/2", "track": "basic", "case_id": "Cavity/2", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/3", "track": "basic", "case_id": "Cavity/3", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulations runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/4", "track": "basic", "case_id": "Cavity/4", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 1.5m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/5", "track": "basic", "case_id": "Cavity/5", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/6", "track": "basic", "case_id": "Cavity/6", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/7", "track": "basic", "case_id": "Cavity/7", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 2m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-03 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/8", "track": "basic", "case_id": "Cavity/8", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-05 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cavity/9", "track": "basic", "case_id": "Cavity/9", "family": "Cavity", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do an incompressible lid driven cavity flow using pisoFoam. The cavity is a square with dimensions normalized to 1 unit on both the x and y axes and very thin in the z-direction (0.1 units) and entire domain scaled down by a factor of 0.1 making it effectively 2D. Use a grid of 20X20 in x and y direction and 1 cell in z-direction(due to the expected 2D flow characteristics). The top wall ('movingWall') moves in the x-direction with a uniform velocity of 3m/s. The 'fixedWalls' have a no-slip boundary condition (velocity equal to zero at the wall). The front and back faces are designated as 'empty'. The simulation runs from time 0 to 10 with a time step of 0.005 units, and results are output every 100 time steps. The viscosity (`nu`) is set as constant with a value of 1e-04 m^2/s. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pisoFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/1", "track": "basic", "case_id": "Cylinder/1", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 0.01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/10", "track": "basic", "case_id": "Cylinder/10", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/2", "track": "basic", "case_id": "Cylinder/2", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/3", "track": "basic", "case_id": "Cylinder/3", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/4", "track": "basic", "case_id": "Cylinder/4", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 1.5m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/5", "track": "basic", "case_id": "Cylinder/5", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/6", "track": "basic", "case_id": "Cylinder/6", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/7", "track": "basic", "case_id": "Cylinder/7", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 2m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-01 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/8", "track": "basic", "case_id": "Cylinder/8", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-03 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:Cylinder/9", "track": "basic", "case_id": "Cylinder/9", "family": "Cylinder", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar offsetcylinder simulation. Use PIMPLE algorithm with a generalized Newtonian model and Cross-Power-Law viscosity for momentum transport, characterized by specific parameters nuInf=10, m=0.4, n=3. Boundary conditions specify a fixed velocity of 3m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls, including the cylinder surface. Use timestep of 0.0025 and output every 0.05. Finaltime is 0.5. use constant viscosity model with nu value of 1e-02 in physical properties. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/1", "track": "basic", "case_id": "counterFlowFlame2D/1", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/10", "track": "basic", "case_id": "counterFlowFlame2D/10", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.4 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/2", "track": "basic", "case_id": "counterFlowFlame2D/2", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.2 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/3", "track": "basic", "case_id": "counterFlowFlame2D/3", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.1 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/4", "track": "basic", "case_id": "counterFlowFlame2D/4", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/5", "track": "basic", "case_id": "counterFlowFlame2D/5", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/6", "track": "basic", "case_id": "counterFlowFlame2D/6", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.3 m/s and velocity of air is -0.3 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/7", "track": "basic", "case_id": "counterFlowFlame2D/7", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.1 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/8", "track": "basic", "case_id": "counterFlowFlame2D/8", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.2 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:counterFlowFlame2D/9", "track": "basic", "case_id": "counterFlowFlame2D/9", "family": "counterFlowFlame2D", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a counterflow flame simulation using OpenFOAM reactingFoam solver, employing a compressible flow solver for detailed combustion modeling. Define the computational domain as a 2D rectangular region with a width of 0.02 meters and a height of 0.02 meters. Use CH4, O2 and N2 as species. Include chemical kinetics using the reaction mechanism. velocity of fuel is 0.4 m/s and velocity of air is -0.3 m/s. Set the simulation runtime from 0 to 0.5 seconds with a write interval of 0.05 seconds and deltaT of 1e-6. Use OpenFOAM-13 with the multicomponentFluid solver module, corresponding to the legacy reactingFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/1", "track": "basic", "case_id": "damBreakWithObstacle/1", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-5 and viscosity of water to be 1e-6. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/10", "track": "basic", "case_id": "damBreakWithObstacle/10", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/2", "track": "basic", "case_id": "damBreakWithObstacle/2", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/3", "track": "basic", "case_id": "damBreakWithObstacle/3", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/4", "track": "basic", "case_id": "damBreakWithObstacle/4", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.0001 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/5", "track": "basic", "case_id": "damBreakWithObstacle/5", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/6", "track": "basic", "case_id": "damBreakWithObstacle/6", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/7", "track": "basic", "case_id": "damBreakWithObstacle/7", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 0.001 and viscosity of water to be 1e-05. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/8", "track": "basic", "case_id": "damBreakWithObstacle/8", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 0.001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:damBreakWithObstacle/9", "track": "basic", "case_id": "damBreakWithObstacle/9", "family": "damBreakWithObstacle", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar dam break with obstacle simulation. user interfoam solver. The domain extent is 1x1x1. Use 32 grid points in all directions. Use density of air to be 1 kg/m3 and density of water to be 1000 kg/m3. Take the viscosity of air to be 1.48e-05 and viscosity of water to be 0.0001. The simulation runs from t=0s to t=0.1s with a timestep of 0.001s and a write interval of 0.02. Use OpenFOAM-13 with the incompressibleVoF solver module, corresponding to the legacy interFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/1", "track": "basic", "case_id": "forwardStep/1", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/10", "track": "basic", "case_id": "forwardStep/10", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.7m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/2", "track": "basic", "case_id": "forwardStep/2", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.1m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/3", "track": "basic", "case_id": "forwardStep/3", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/4", "track": "basic", "case_id": "forwardStep/4", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.5m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/5", "track": "basic", "case_id": "forwardStep/5", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.7m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/6", "track": "basic", "case_id": "forwardStep/6", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 1.9m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/7", "track": "basic", "case_id": "forwardStep/7", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.1m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/8", "track": "basic", "case_id": "forwardStep/8", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.3m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:forwardStep/9", "track": "basic", "case_id": "forwardStep/9", "family": "forwardStep", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a laminar, compressible flow over a forward-facing step using the rhoCentralFoam solver. Boundary conditions include a fixed velocity of 2.5m/s and temperature of 1 K at the inlet and slip conditions on the obstacle. Use timestep of 0.002 and output every 0.1. Finaltime is 4. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/1", "track": "basic", "case_id": "obliqueShock/1", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperature of 1.25853, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/10", "track": "basic", "case_id": "obliqueShock/10", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (4.0,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/2", "track": "basic", "case_id": "obliqueShock/2", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (3.0,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/3", "track": "basic", "case_id": "obliqueShock/3", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 3.5 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/4", "track": "basic", "case_id": "obliqueShock/4", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of 1.0 K and top boundary temperaure of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/5", "track": "basic", "case_id": "obliqueShock/5", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 3.5 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/6", "track": "basic", "case_id": "obliqueShock/6", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (3.0,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/7", "track": "basic", "case_id": "obliqueShock/7", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (3.5,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 1.25853 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/8", "track": "basic", "case_id": "obliqueShock/8", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 2.9 m/s and top velocity of (2.61933,-0.50632,0.0) m/s. Use an inlet temperature of  1.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:obliqueShock/9", "track": "basic", "case_id": "obliqueShock/9", "family": "obliqueShock", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a 2D oblique shock wave simulation using OpenFOAM with the rhoCentralFoam solver. The computational domain spans 4.1 m x 1.0 m x 0.1 m. Use inlet velocity of 4.0 m/s and top velocity of (3.5,-0.50632,0.0) m/s. Use an inlet temperature of  2.0 K and top boundary temperature of 2.0 K, and an inlet pressure of 1.0 Pa. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use a time step of 0.0025 seconds, output results every 1.0 seconds, and run the simulation until a final time of 10 seconds. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/1", "track": "basic", "case_id": "pitzDaily/1", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 10m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-5. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/10", "track": "basic", "case_id": "pitzDaily/10", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/2", "track": "basic", "case_id": "pitzDaily/2", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/3", "track": "basic", "case_id": "pitzDaily/3", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/4", "track": "basic", "case_id": "pitzDaily/4", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 15m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/5", "track": "basic", "case_id": "pitzDaily/5", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/6", "track": "basic", "case_id": "pitzDaily/6", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/7", "track": "basic", "case_id": "pitzDaily/7", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 20m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-03. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/8", "track": "basic", "case_id": "pitzDaily/8", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-05. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:pitzDaily/9", "track": "basic", "case_id": "pitzDaily/9", "family": "pitzDaily", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a Reynolds-Averaged Simulation (RAS) pitzdaily simulation. Use PIMPLE algorithm. The domain is a 2D millimeter-scale channel geometry. Boundary conditions specify a fixed velocity of 25m/s at the inlet (left),zero gradient pressure at the outlet (right), and no-slip conditions for walls. Use timestep of 0.0001 and output every 0.01. Finaltime is 0.3. use nu value of 1e-04. Use OpenFOAM-13 with the incompressibleFluid solver module, corresponding to the legacy pimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/1", "track": "basic", "case_id": "shallowWaterWithSquareBump/1", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.01 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/10", "track": "basic", "case_id": "shallowWaterWithSquareBump/10", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.1 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/2", "track": "basic", "case_id": "shallowWaterWithSquareBump/2", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.02 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/3", "track": "basic", "case_id": "shallowWaterWithSquareBump/3", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.03 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/4", "track": "basic", "case_id": "shallowWaterWithSquareBump/4", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.04 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/5", "track": "basic", "case_id": "shallowWaterWithSquareBump/5", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.05 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/6", "track": "basic", "case_id": "shallowWaterWithSquareBump/6", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.06 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/7", "track": "basic", "case_id": "shallowWaterWithSquareBump/7", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.07 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/8", "track": "basic", "case_id": "shallowWaterWithSquareBump/8", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.08 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:shallowWaterWithSquareBump/9", "track": "basic", "case_id": "shallowWaterWithSquareBump/9", "family": "shallowWaterWithSquareBump", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "do a shallow water simulation over a square bump using the shallowWaterFoam solver. The domain spans 1 x 1 x 0.1, discretized into 20 x 20 x 1 grid points. The simulation initializes with a uniform water depth of 0.09 m and a uniform momentum field of (0.001,0,0). The simulation runs from 0 s to 100 s with a timestep of 0.1 s and writes results every 1 s. Use OpenFOAM-13 legacy executable shallowWaterFoam; this case is not a foamRun solver module case.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/1", "track": "basic", "case_id": "squareBend/1", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/10", "track": "basic", "case_id": "squareBend/10", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 1e-4. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/2", "track": "basic", "case_id": "squareBend/2", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1500. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/3", "track": "basic", "case_id": "squareBend/3", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/4", "track": "basic", "case_id": "squareBend/4", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/5", "track": "basic", "case_id": "squareBend/5", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/6", "track": "basic", "case_id": "squareBend/6", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1100. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 1.0. Use mu value of 2.5e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/7", "track": "basic", "case_id": "squareBend/7", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1100. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 5.0e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/8", "track": "basic", "case_id": "squareBend/8", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 5.0e-5. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:squareBend/9", "track": "basic", "case_id": "squareBend/9", "family": "squareBend", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Conduct a 3D squarebend flow simulation using OpenFOAM. The computational domain includes multiple regions, with vertices defined as inlet points at (-50, 25, 25) and (-50, 25, -25), outlet points at (-500, -75, 25) and (-500, -75, -25), and mid-bend points like (25, 0, 25) and (25, 0, -25). Follow the same geomtery as the tutorial. Use a start time of 0 seconds, an end time of 500 seconds, a time step of 1 second, and write results every 100 seconds. Use a massflow rate inlet of 0.5 with turbulentBL profile. Outlet is pressureInletOutletVelocity. Temperature has an inlet value of 1000. Pressure inlet has a value of 110000. use kepsilon turbulence model. Use rhoSimpleFoam solver. Use Pr value of 0.71. Use mu value of 1e-4. Use OpenFOAM-13 with the fluid solver module, corresponding to the legacy rhoSimpleFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/1", "track": "basic", "case_id": "wedge/1", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 5 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/10", "track": "basic", "case_id": "wedge/10", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/2", "track": "basic", "case_id": "wedge/2", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 1 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/3", "track": "basic", "case_id": "wedge/3", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/4", "track": "basic", "case_id": "wedge/4", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.0001 seconds. The results are written every 0.02 seconds. The inlet velocity is 10 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/5", "track": "basic", "case_id": "wedge/5", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/6", "track": "basic", "case_id": "wedge/6", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/7", "track": "basic", "case_id": "wedge/7", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 15 m/s, inlet temperature is 2 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/8", "track": "basic", "case_id": "wedge/8", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
+{"task_id": "basic:wedge/9", "track": "basic", "case_id": "wedge/9", "family": "wedge", "task_origin": "FoamBench (upstream; adapted for OpenFOAM 13)", "usr_requirement": "Perform a 2D supersonic flow simulation over a wedge. Create a 3D geometry spanning from -0.15242 m to 0.3048 m in the x-direction, 0 m to 0.1524 m in the y-direction, and -0.005 m to 0.005 m in the z-direction. The simulation starts at 0.0 seconds and runs until 0.2 seconds with a time step (deltaT) of 0.00005 seconds. The results are written every 0.02 seconds. The inlet velocity is 20 m/s, inlet temperature is 3 K and inlet pressure is 1 Pa. The wedge boundary uses slip boundary condition for velocity. Use normalized thermodynamic properties where molWeight is set to 11640.3, Cp is 2.5, Pr is 1.0, and dynamic viscosity mu is 0. This corresponds to a gas constant R of 0.7143 and a specific heat ratio of 1.4. Use rhoCentralFoam solver. Use OpenFOAM-13 with the shockFluid solver module, corresponding to the legacy rhoCentralFoam application.", "external_asset_ids": []}
diff --git a/data/extended.jsonl b/data/extended.jsonl
new file mode 100644
index 0000000000000000000000000000000000000000..8304aef1deb361d9744bf18040fe3af1653cd82b
--- /dev/null
+++ b/data/extended.jsonl
@@ -0,0 +1,100 @@
+{"task_id": "extended:ERCOFTA_pump/1", "track": "extended", "case_id": "ERCOFTA_pump/1", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady incompressible ERCOFTA pump reference case using OpenFOAM-13 with foamRun -solver incompressibleFluid, using the tutorial-style MRF rotating-machine setup with a rotor cellZone, inlet/outlet boundaries, and wall patches for the blade and shroud surfaces. Keep the design-speed rotation rate and the baseline RANS closure fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use an incompressible liquid with kinematic viscosity 1e-6 m2/s, a volumetric inlet flow of 0.03473 m3/s and zero-gauge outlet pressure. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/10", "track": "extended", "case_id": "ERCOFTA_pump/10", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady compressible ERCOFTA rotating-machine surrogate using foamRun -solver fluid. Change only the uniform rectangular surrogate mesh from 24x8x16 to 48x16x32; retain omega=-20, RAS kOmegaSST, thermophysical fields, boundaries, steady discretisation, and run controls. This is the fine-mesh resolution variant, not a claim of supplied double-row blade geometry. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/2", "track": "extended", "case_id": "ERCOFTA_pump/2", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady compressible ERCOFTA pump reference case using OpenFOAM-13 with foamRun -solver fluid, keeping the tutorial-style rotating-region setup, the rotor cellZone, inlet/outlet boundaries, and the baseline RANS closure fixed. Retain the compressible thermophysical settings and the design-speed rotation rate. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/3", "track": "extended", "case_id": "ERCOFTA_pump/3", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-region setup as the baseline but changing only the rotating speed away from the design RPM. Keep the rotor cellZone, boundary layout, turbulence model, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -25 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/4", "track": "extended", "case_id": "ERCOFTA_pump/4", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the steady compressible ERCOFTA rotating-region surrogate with foamRun -solver fluid and change only the OUTLET fixed pressure from the 101325 Pa baseline to 120000 Pa. Keep the rotor cellZone, omega=-20, kOmegaSST, thermophysical model, mesh, boundaries, steady SIMPLE settings, endTime=0.001, deltaT=5e-7, and writeInterval=1 fixed. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 120000 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/5", "track": "extended", "case_id": "ERCOFTA_pump/5", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transient compressible ERCOFTA rotating-region surrogate using foamRun -solver fluid with the same perfect-gas thermophysical model, inlet/outlet conditions, U field, omega=-20, mesh, and rotor cellZone as the compressible baseline. Change only the temporal/turbulence treatment to Euler + PIMPLE with LES kOmegaSSTDES; use endTime=0.001, deltaT=1e-6, and writeInterval=1. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/6", "track": "extended", "case_id": "ERCOFTA_pump/6", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-region setup as the baseline but switching only the turbulence model to kEpsilon. Keep the rotor cellZone, rotating speed, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/7", "track": "extended", "case_id": "ERCOFTA_pump/7", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady compressible ERCOFTA rotating-region surrogate with foamRun -solver fluid as a rotor-zone-extent sensitivity case. Extend only the boxToCell rotor region from the baseline x=0..0.3 to x=0..0.45 while retaining omega=-20, RAS kOmegaSST, thermophysical fields, mesh, boundary conditions, steady SIMPLE settings, endTime=0.001, deltaT=5e-7, and writeInterval=1. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/8", "track": "extended", "case_id": "ERCOFTA_pump/8", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady compressible ERCOFTA rotating-region surrogate using foamRun -solver fluid with omega=-15, retaining the baseline kOmegaSST, perfect-gas thermophysical model, rotor zone, mesh, boundaries, steady SIMPLE controls, and post-processing. This is the low-speed companion to omega=-20 baseline and omega=-25 variant. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -15 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:ERCOFTA_pump/9", "track": "extended", "case_id": "ERCOFTA_pump/9", "family": "ERCOFTA_pump", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transient ERCOFTA pump case using OpenFOAM-13 with foamRun -solver fluid, following the same tutorial-derived rotating-machinery setup as the baseline but using the legacy rhoPimpleFoam-style transient PIMPLE coupling. Keep the rotor cellZone, rotating speed, turbulence model, and all other settings fixed. Run from t=0 to t=0.001 with deltaT=5e-7 and write every time step. Treat this as the supplied rectangular rotating-region surrogate, not as an unspecified blade-resolved pump: the domain is 0.6 x 0.25 x 0.2 m, and the baseline rotor zone occupies x=0 to 0.3 m. Use angular velocity -20 rad/s about the z-axis. Use calorically perfect air at 300 K with molecular weight 28.964, Cp=1004.7 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.72; set the inlet mass flow rate to 0.03473 kg/s and the outlet pressure to 101325 Pa. Preserve the rotating and stationary wall roles.", "external_asset_ids": []}
+{"task_id": "extended:MRF_stirredReactor/1", "track": "extended", "case_id": "MRF_stirredReactor/1", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible laminar stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use a tutorial-derived Rushton stirred tank setup with the tank, shaft, impeller/stirrer, rotating zone, and stationary baffles where applicable. Configure a rotating MRF cellZone for the impeller region at 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and laminar momentum transport. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Include stirrer torque or power monitoring when supported by the tutorial-derived setup. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/10", "track": "extended", "case_id": "MRF_stirredReactor/10", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a two-phase liquid-liquid stirred-reactor MRF benchmark using water and oil with incompressibleVoF. Initialise a finite oil layer over a water region using OpenFOAM-13 setFields syntax, use zero gravity and retain p_rgh, interface compression, adaptive time stepping, and a 100 rpm MRF rotor. This is the water/oil variant, distinct from the single-phase laminar, turbulence, baffle, rheology, NCC, and transient variants. Use an eight-sector rotor-stator vessel with outer radius 0.10 m, rotor-tip radius 0.05 m, stator-tip radius 0.07 m and a 0.01 m quasi-2D thickness. Water has density 1000 kg/m3 and kinematic viscosity 1e-4 m2/s; oil has density 500 kg/m3 and the same viscosity; surface tension is 0.05 N/m and gravity is zero. Initially the lower portion up to z=0.0025 m is water and the rest is oil.", "external_asset_ids": []}
+{"task_id": "extended:MRF_stirredReactor/2", "track": "extended", "case_id": "MRF_stirredReactor/2", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible turbulent stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone for the impeller region and stationary tank/baffle walls. Set the impeller speed to 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Include stirrer torque or power monitoring when supported by the tutorial-derived setup. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/3", "track": "extended", "case_id": "MRF_stirredReactor/3", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible turbulent stirred-reactor benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to a steady simpleFoam-style MRF calculation. Use the same tutorial-derived Rushton stirred tank geometry and rotating MRF cellZone as the kEpsilon baseline. Set the impeller speed to 100 rpm. Use a Newtonian fluid with constant kinematic viscosity and the RAS kOmegaSST turbulence model. Run steady-state SIMPLE iterations from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Keep the mesh, boundary conditions, and MRF rotating-zone setup consistent with the kEpsilon case so the turbulence-model effect can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/4", "track": "extended", "case_id": "MRF_stirredReactor/4", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible stirred-reactor MRF speed-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank geometry with a rotating MRF cellZone and stationary tank/baffle walls. Use a Newtonian fluid with constant kinematic viscosity and the RAS kEpsilon turbulence model. Run an impeller-speed comparison for 50 rpm, 100 rpm, and 200 rpm by changing the rotating-zone omega value while keeping the mesh, boundary conditions, and numerical schemes fixed. Run each speed case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/5", "track": "extended", "case_id": "MRF_stirredReactor/5", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible stirred-reactor MRF baffle-sensitivity benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to steady simpleFoam-style calculations. Use the tutorial-derived Rushton stirred tank setup and compare a baffled tank configuration with four stationary baffles against an otherwise identical unbaffled tank configuration. Use the same rotating MRF cellZone, impeller geometry, Newtonian constant-viscosity fluid, 100 rpm impeller speed, and RAS kEpsilon turbulence model in both configurations. Run each case from t=0 to t=1000 with deltaT=1 and write results every 100 time steps so the baffle effect on flow and stirrer power can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/6", "track": "extended", "case_id": "MRF_stirredReactor/6", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible stirred-reactor MRF benchmark for a polymer-like non-Newtonian liquid using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use the tutorial-derived Rushton stirred tank geometry with the rotating MRF cellZone, impeller, shaft, and baffles. Configure a generalised-Newtonian CrossPowerLaw viscosity model for the liquid instead of a constant-viscosity Newtonian model. Use an impeller speed of 100 rpm and a steady simpleFoam-style MRF formulation. Run from t=0 to t=1000 with deltaT=1 and write results every 100 time steps. Keep the mesh and boundary conditions consistent with the Newtonian MRF baseline so the rheology effect can be compared. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. For the non-Newtonian variant use the Cross-Power-Law values nu0=0.01 m2/s, nuInf=10 m2/s, m=0.4 s and n=3. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/7", "track": "extended", "case_id": "MRF_stirredReactor/7", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a stirred-reactor comparison between a steady MRF approximation and a sliding-mesh/NCC rotating-impeller calculation using OpenFOAM-13 with foamRun -solver incompressibleFluid. Use tutorial-derived Rushton stirred tank setups for both cases, keeping the tank, baffles, impeller geometry, fluid properties, turbulence model, and impeller speed consistent. For the MRF case, use the rotating MRF cellZone formulation. For the sliding-mesh case, use the corresponding non-conformal coupling or dynamic-mesh tutorial workflow for the rotating impeller region. Use a Newtonian fluid, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Compare the resulting flow field and stirrer power or torque outputs. Extend the full run to t=100 with writeInterval=10 so the sliding-mesh power reaches a stable endpoint. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/8", "track": "extended", "case_id": "MRF_stirredReactor/8", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady incompressible stirred-reactor MRF mesh-refinement benchmark using foamRun -solver incompressibleFluid with RAS kEpsilon, 100 rpm, the same Rushton geometry, baffles, fluid properties, steady controls, power functions, and boundary conditions as the baseline. Change only the structured tank mesh factor from 1 to 2. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:MRF_stirredReactor/9", "track": "extended", "case_id": "MRF_stirredReactor/9", "family": "MRF_stirredReactor", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transient incompressible stirred-reactor MRF benchmark using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy pimpleFoam application. Use the same tutorial-derived Rushton stirred tank geometry and rotating MRF cellZone as the steady MRF baseline. Use a Newtonian fluid with constant kinematic viscosity, an impeller speed of 100 rpm, and the RAS kEpsilon turbulence model. Use transient time discretisation with PIMPLE pressure-velocity coupling instead of steady SIMPLE. Run from t=0 to t=1 with deltaT=0.001 and write results every 100 time steps. Keep the mesh, boundary conditions, and MRF rotating-zone setup consistent with the steady MRF case. Use the supplied Rushton geometry assets (simpleRushtonMRF/stirrer4, simpleRushtonMRF/stirrer6, simpleRushtonMRF/baffles) rather than inventing a different impeller. The tank diameter is 1.0 m, its height is 1.2 m, the impeller radius is 0.15 m and the rotating-zone radius is 0.20 m. Use a Newtonian liquid with kinematic viscosity 1e-6 m2/s. Maintain a small through-flow with mean inlet velocity 1e-3 m/s and an open pressure outlet. Keep the tank, shaft, impeller and baffle surfaces no-slip except where the selected rotating-frame formulation requires otherwise.", "external_asset_ids": ["simpleRushtonMRF/stirrer4", "simpleRushtonMRF/stirrer6", "simpleRushtonMRF/baffles"]}
+{"task_id": "extended:aerofoilNACA0012/1", "track": "extended", "case_id": "aerofoilNACA0012/1", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a low-subsonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.15 at zero angle of attack; set speed=52 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/10", "track": "extended", "case_id": "aerofoilNACA0012/10", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady compressible NACA0012 aerofoil turbulence variant using foamRun -solver fluid with the 2D structured/snappy geometry, SpalartAllmaras RAS, steady SIMPLE controls, and the same Mach 0.5, AoA=0, mesh, thermophysical fields, and forceCoeffs workflow as the baseline. This is the economical 2D SA-RANS alternative to the baseline kOmegaSST case; it does not claim DDES. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/2", "track": "extended", "case_id": "aerofoilNACA0012/2", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a subsonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at zero angle of attack; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/3", "track": "extended", "case_id": "aerofoilNACA0012/3", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transonic-onset NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.7 at zero angle of attack; set speed=242 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/4", "track": "extended", "case_id": "aerofoilNACA0012/4", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transonic NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.8 at zero angle of attack; set speed=277 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/5", "track": "extended", "case_id": "aerofoilNACA0012/5", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a negative-five-degree NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=-5 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=-5 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/6", "track": "extended", "case_id": "aerofoilNACA0012/6", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a five-degree angle-of-attack NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=5 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=5 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=1000; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/7", "track": "extended", "case_id": "aerofoilNACA0012/7", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a ten-degree angle-of-attack NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid. Use the provided NACA0012 aerofoil geometry for mesh generation. The target angle condition is AoA=10 degrees at Ma=0.5; set speed=173 m/s and angleOfAttack=10 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Run from t=0 to t=1500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/8", "track": "extended", "case_id": "aerofoilNACA0012/8", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid and a snappyHexMesh multi-level refinement strategy. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at AoA=0 degrees; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model. Generate a background mesh and apply snappyHexMesh refinement around the aerofoil surface, near-field region, and downstream wake while preserving extruded front/back constraint patches for a quasi-2D aerofoil calculation. Run from t=0 to t=500; deltaT=1; write results every 50 time steps using writeControl=timeStep. Include the OpenFOAM case configuration, initial and boundary fields, blockMesh/snappyHexMesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:aerofoilNACA0012/9", "track": "extended", "case_id": "aerofoilNACA0012/9", "family": "aerofoilNACA0012", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transient compressible NACA0012 aerofoil benchmark using OpenFOAM-13 with foamRun -solver fluid, corresponding to the legacy rhoPimpleFoam-style workflow. Use the provided NACA0012 aerofoil geometry for mesh generation. The target condition is Ma=0.5 at AoA=0 degrees; set speed=173 m/s and angleOfAttack=0 degrees in 0/U. Use the kOmegaSST RANS turbulence model and the standard projected NACA0012 mesh with extruded front/back constraint patches. Use transient time discretisation and PIMPLE pressure-velocity coupling suitable for the rhoPimpleFoam replacement path. Run from t=0 to t=0.15; deltaT=2e-5; write results every 0.001 simulation-time units using writeControl=adjustableRunTime. Include the OpenFOAM case configuration, initial and boundary fields, mesh dictionaries, force coefficient function object, and the external geometry path needed to run the case. Treat the supplied NACA0012 surface as a unit-chord aerofoil. Use calorically perfect air at 298 K and 100000 Pa with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.82e-5 Pa s and Pr=0.71; impose a no-slip aerofoil and far-field conditions. Use a 1 m reference chord and unit reference span for force coefficients.", "external_asset_ids": ["naca0012/NACA0012"]}
+{"task_id": "extended:compressibleBubbleCollapse/1", "track": "extended", "case_id": "compressibleBubbleCollapse/1", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. This is the baseline single-bubble case with a circular gas bubble of radius 50um centered in the domain at 5MPa ambient pressure, using the same 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport as the shared baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/10", "track": "extended", "case_id": "compressibleBubbleCollapse/10", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the number of bubbles by introducing a second identical 50um bubble so the two bubbles interact, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the single-bubble baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Place the second 50 um bubble 0.15 mm from the first in the radial direction.", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/2", "track": "extended", "case_id": "compressibleBubbleCollapse/2", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble radius, using two radius subcases of 100um and 200um, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, bubble center, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the 50um baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/3", "track": "extended", "case_id": "compressibleBubbleCollapse/3", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the ambient pressure, using a weak-collapse branch at 2MPa and a strong-collapse branch at 10MPa, while keeping the 50um single bubble, centered placement, 2D 10mm-high domain, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/4", "track": "extended", "case_id": "compressibleBubbleCollapse/4", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the bubble-center distance from the solid wall, placing the 50um bubble in a near-wall configuration, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Place the bubble centre 0.20 mm above the bottom wall.", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/5", "track": "extended", "case_id": "compressibleBubbleCollapse/5", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the initial gas-bubble shape, replacing the circular 50um baseline bubble with a stepped/asymmetric axis-aligned rectangular initial contour represented by two boxToCell selections at the same center location, while keeping the 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport unchanged. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K). Form the asymmetric bubble from two overlapping rectangles: one spanning radial coordinate -53.79 to 26.21 um and height 4.9625 to 5.0375 mm, and the second spanning 26.21 to 63.21 um and height 4.975 to 5.025 mm.", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/6", "track": "extended", "case_id": "compressibleBubbleCollapse/6", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the gas-liquid density ratio, using a lighter-gas branch by lowering the air density while keeping the liquid model, the 50um bubble geometry, the 2D 10mm-high domain, the 5MPa ambient pressure, and the interfaceCompression + vanLeer VOF transport fixed to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 14.48 and Cp=2009.406 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/7", "track": "extended", "case_id": "compressibleBubbleCollapse/7", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver compressibleVoF. Change only the mesh strategy by enabling AMR around the gas-liquid interface with dynamicRefineFvMesh, while keeping the 50um single bubble, 2D 10mm-high domain, 5MPa ambient pressure, water/air phases, compressible perfectFluid liquid equation of state, gamma=1.4 air, and interfaceCompression + vanLeer VOF transport identical to the baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/8", "track": "extended", "case_id": "compressibleBubbleCollapse/8", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the fixed uniform fine-mesh compressible bubble-collapse baseline using foamRun -solver compressibleVoF. Keep the 50 um bubble, 5 MPa pressure, thermophysical model, interface scheme, and controls fixed while refining the uniform base mesh from 200x1x200 to 400x1x400. This is the fixed-grid resolution counterpart to the adaptive-AMR variant. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For water use the perfect-fluid relation with rho0=998 kg/m3, R=100000 J/kg and Cv=4195 J/(kg K); for the gas use a perfect-gas model with molecular weight 28.96 and Cp=1004.5 J/(kg K).", "external_asset_ids": []}
+{"task_id": "extended:compressibleBubbleCollapse/9", "track": "extended", "case_id": "compressibleBubbleCollapse/9", "family": "compressibleBubbleCollapse", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible two-phase bubble-collapse benchmark using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Change only the solver family and compressibility treatment for an incompressible VOF comparison, while keeping the same 50um bubble placement, 2D 10mm-high domain, water/air interface geometry, and as much of the baseline setup as the solver allows. This branch is the incompressible interFoam-style reference against the compressible bubble-collapse baseline. Run from t=0 to t=1e-7; deltaT=1e-10; write results every 1e-8 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.3, maxAlphaCo=1, maxDeltaT=2e-9. Use a 5-degree axisymmetric wedge domain with radius and height both 10 mm. The bottom is a solid wall, the top maintains the ambient pressure and the outer radial boundary is non-penetrating. Initially the liquid and gas are at 300 K, the gas pressure is 3550 Pa, gravity is zero and surface tension is neglected. For this incompressible comparison use water rho=998 kg/m3 and nu=3.653e-7 m2/s, air rho=1.2 kg/m3 and nu=1.533e-5 m2/s.", "external_asset_ids": []}
+{"task_id": "extended:drivaerFastback/1", "track": "extended", "case_id": "drivaerFastback/1", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. DrivAer fastback baseline at 100 km/h with static ground, rotatingWallVelocity wheels, and kOmegaSST. Set Uinlet to 27.7778 m/s. Use lightweight snappy mesh level 2. Run from t=0 to t=100; deltaT=1; write results every 50 using writeControl=timeStep. Enable forceCoeffs for aerodynamic coefficients. Keep geometry referenced by DrivAer body/frontWheels/rearWheels triSurface names without embedding solver results. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/10", "track": "extended", "case_id": "drivaerFastback/10", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a transient 3D DrivAer fastback DDES benchmark using foamRun -solver incompressibleFluid with LES SpalartAllmarasDDES, Euler time discretisation, PIMPLE coupling, Uinlet=27.7778 m/s, rotating wheels, static ground, and the supplied geometry. Use endTime=10, deltaT=0.01, writeControl=timeStep, and writeInterval=10; analyse the final transient window rather than treating this as a steady simpleFoam run. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/2", "track": "extended", "case_id": "drivaerFastback/2", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Run the supplied DrivAer fastback surrogate with foamRun -solver incompressibleFluid at the baseline 27.7778 m/s, but use a 60-cell streamwise background mesh instead of 40 cells. Keep static ground, rotatingWallVelocity wheels, kOmegaSST, forceCoeffs, and run controls unchanged; this is the medium-resolution variant. For Q2 evidence, continue the validated decomposed run to t=200 and merge restart-segment forceCoeffs history. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/3", "track": "extended", "case_id": "drivaerFastback/3", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Run the supplied DrivAer fastback surrogate with foamRun -solver incompressibleFluid using the baseline Uinlet=27.7778 m/s and an 80-cell streamwise background mesh. Keep static ground, rotatingWallVelocity wheels, kOmegaSST, forceCoeffs, and run controls unchanged. This is the fine-mesh third level after the 40-cell baseline and 60-cell variant. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/4", "track": "extended", "case_id": "drivaerFastback/4", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the vehicle speed to 120 km/h relative to the Fastback baseline. Set Uinlet to 33.3333 m/s and compute wheelSpeed from Uinlet/wheelRadius; keep the fastback geometry, static ground, rotatingWallVelocity wheels, snappy mesh, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/5", "track": "extended", "case_id": "drivaerFastback/5", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the vehicle speed to 80 km/h relative to the Fastback baseline. Set Uinlet to 22.2222 m/s and compute wheelSpeed from Uinlet/wheelRadius; keep the fastback geometry, static ground, rotatingWallVelocity wheels, snappy mesh, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/6", "track": "extended", "case_id": "drivaerFastback/6", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the wheel-rotation method to an MRF-style treatment for the front and rear wheels, while keeping the fastback geometry, 100 km/h inflow, static ground, mesh setup, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/7", "track": "extended", "case_id": "drivaerFastback/7", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Change only the ground boundary condition to a moving ground with velocity Uinlet, while keeping the fastback geometry, 100 km/h inflow, rotatingWallVelocity wheels, mesh setup, kOmegaSST turbulence, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/8", "track": "extended", "case_id": "drivaerFastback/8", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Use the standard kEpsilon turbulence model, while keeping the fastback geometry, 100 km/h inflow, wheel treatment, mesh setup, run controls, and forceCoeffs post-processing consistent with the baseline. For Q2 evidence, continue the validated decomposed run to t=200 and merge restart-segment forceCoeffs history. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:drivaerFastback/9", "track": "extended", "case_id": "drivaerFastback/9", "family": "drivaerFastback", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform an incompressible external-aerodynamics simulation of the DrivAer fastback model using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application. Use the standard RAS kOmega turbulence model instead of the baseline kOmegaSST model, while keeping the fastback geometry, 100 km/h inflow, wheel treatment, mesh setup, run controls, and forceCoeffs post-processing consistent with the baseline. Use the supplied body and wheel assets (drivaerFastback/body, drivaerFastback/frontWheels, drivaerFastback/rearWheels) without altering their scale. Model air with kinematic viscosity 1.5e-5 m2/s. Use wheel radius 0.318 m and wheelbase 2.786 m; for rotating wheels set angular speed consistently from vehicle speed divided by wheel radius.", "external_asset_ids": ["drivaerFastback/body", "drivaerFastback/frontWheels", "drivaerFastback/rearWheels"]}
+{"task_id": "extended:nozzleCDV/1", "track": "extended", "case_id": "nozzleCDV/1", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. CDV baseline transonic case with throat Mach number approximately 1.0. Use this as the reference structured-mesh, laminar, fluid-solver configuration. Keep the CDV geometry, structured 2D mesh, thermophysical model, laminar model, physical flow condition, and pressure-density convection format div(phi,(p|rho)) unchanged unless this variant explicitly changes that one main variable. Run as transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/10", "track": "extended", "case_id": "nozzleCDV/10", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady 2D compressible CDV nozzle turbulence comparison using foamRun -solver fluid with RAS kOmegaSST. Keep the supplied structured CDV mesh, thermophysical model, boundary conditions, endTime=0.005, deltaT=1e-6, and sampling fixed; this is the 2D RANS turbulence variant, replacing the physically unsuitable quasi-2D DDES design. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/2", "track": "extended", "case_id": "nozzleCDV/2", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the CDV baseline compressible nozzle case with foamRun -solver fluid, using the supplied structured CDV geometry and a throat-refined mesh. Change only the first converging-section cell count from 40 to 80 (with all solver, thermophysical, flow, boundary, and run settings unchanged); this is the mesh-resolution variant. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/3", "track": "extended", "case_id": "nozzleCDV/3", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the supplied CDV compressible nozzle case with foamRun -solver fluid at a reduced outlet back pressure of 95000 Pa. Keep the CDV geometry, mesh, solver, thermophysical model, inlet state, discretisation, and run controls fixed; this is the back-pressure variant distinct from the mesh-refined nozzleCDV/2 case. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 95000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/4", "track": "extended", "case_id": "nozzleCDV/4", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Back-pressure scan for subsonic, transonic, and supersonic CDV response. Change only the outlet static pressure by running three otherwise identical subcases with pBack=101325, 90000, and 35000 Pa; keep inlet velocity, geometry, mesh, solver, turbulence model, and schemes fixed. Run each subcase from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. For every branch use a 300 K inlet and the 320 m/s baseline inlet speed; vary only the outlet pressure values stated above. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/5", "track": "extended", "case_id": "nozzleCDV/5", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Mesh-type variant for the design-table comparison between the structured blockMesh baseline and a non-structured/polyhedral mesh. Change only the mesh representation by starting from the same CDV blockMesh geometry and converting the hex mesh with polyDualMesh using featureAngle=70; keep the geometry envelope, solver, laminar model, target flow condition, boundary conditions, and numerical schemes otherwise fixed. Run transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Compare this case against nozzleCDV/1 as the structured-mesh reference. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/6", "track": "extended", "case_id": "nozzleCDV/6", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Discretisation-format variant from the design table: run an upwind stabilisation stage first, then switch to the stable higher-order linear/limited convection treatment used by the baseline for the remaining time. Change only the convection discretisation by running with system/fvSchemes.upwind to t=0.0025 and then continuing from latestTime with system/fvSchemes.limitedLinear to t=0.005; keep geometry, mesh, solver, laminar model, flow target, and boundary conditions fixed. Write results every 0.001 simulation-time units. Use distinct upwind and limitedLinear log suffixes so the second stage is executed rather than skipped by RunFunctions. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and a static outlet pressure of 90000 Pa. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/7", "track": "extended", "case_id": "nozzleCDV/7", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Boundary-condition variant from the design table using total pressure and total temperature at the inlet with a static-pressure outlet. Change only the inlet/outlet boundary-condition formulation; keep the CDV geometry, structured 2D mesh, solver, laminar model, target flow condition, and numerical schemes fixed. Run transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-6; write results every 0.001 simulation-time units. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use inlet total pressure 350000 Pa and total temperature 300 K, with a 90000 Pa static-pressure outlet. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/8", "track": "extended", "case_id": "nozzleCDV/8", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver shockFluid. Solver-comparison variant using shockFluid, the OpenFOAM-13 replacement for the legacy rhoCentralFoam central-upwind shock-capturing solver. Change only the solver family and its required convection schemes; keep geometry, mesh, target inlet speed, inlet thermodynamic state, wall treatment, and turbulence model fixed while using shockFluid-compatible outlet extrapolation. Keep the CDV geometry, structured 2D mesh, thermophysical model, laminar model, physical flow condition, and pressure-density convection format div(phi,(p|rho)) unchanged unless this variant explicitly changes that one main variable. Run as transient PIMPLE-style iterations from t=0 to t=0.005; deltaT=1e-7; write results every 0.001 simulation-time units using a fixed-step shockFluid configuration aligned with the tutorial-style solver setup. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use a 320 m/s, 300 K inlet and the 90000 Pa baseline pressure level, with shock-compatible extrapolation at the outlet. Use no-slip nozzle walls.", "external_asset_ids": []}
+{"task_id": "extended:nozzleCDV/9", "track": "extended", "case_id": "nozzleCDV/9", "family": "nozzleCDV", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible converging-diverging nozzle benchmark using OpenFOAM-13 with foamRun -solver fluid. Dimension variant from the design table: use a true 2D axisymmetric CDV nozzle simplification represented by a small-angle wedge mesh, not a planar half-channel symmetry-plane approximation. Preserve the axial converging-diverging radius profile, collapse the centerline to an axis patch with empty field conditions, and use front/back wedge patches so the OpenFOAM wedge formulation includes the cylindrical-coordinate geometric effect. Use a standard compressible nozzle boundary-condition formulation with totalPressure p0=160000 Pa and totalTemperature T0=300 K at the inlet, pressureInletOutletVelocity for the open velocity boundaries, and a static-pressure outlet p=90000 Pa. Use slip walls for the inviscid/laminar axisymmetric nozzle-wall idealisation. Run transient PIMPLE pseudo-time integration to a quasi-steady converged state from t=0 to t=0.1 with fixed deltaT=1e-5, adjustTimeStep=no, maxCo=0.5, maxDeltaT=1e-5, and writeInterval=0.02. Use a unit-length nozzle with axial stations at x=0, 0.4, 0.6 and 1.0 m and corresponding half-heights 0.20, 0.08, 0.08 and 0.20 m. Model calorically perfect air with molecular weight 28.9, Cp=1005 J/(kg K), viscosity 1.8e-5 Pa s and Pr=0.7. Use the axisymmetric wedge interpretation and the total-pressure/total-temperature and back-pressure values already stated above.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/1", "track": "extended", "case_id": "riemann2D/1", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Configure and run the CFD-China four-quadrant two-dimensional Riemann problem in OpenFOAM-13 using foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use the square domain [-5,5] x [-5,5] on a uniform 800 x 800 mesh with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov central-upwind flux, vanAlbada reconstruction for rho and T, and vanAlbadaV reconstruction for U. Use zero-gradient conditions on the four outer sides and empty front/back patches. Advance to t=1.5 with adaptive time stepping and maxCo=0.2, writing results every 0.15 time units. Provide time-resolved density and pressure contours together with final rho and p profiles along the horizontal and vertical centre-lines.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/10", "track": "extended", "case_id": "riemann2D/10", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Evaluate restart fidelity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use a uniform 600 x 600 mesh over [-5,5] x [-5,5] with one cell through the empty direction, the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries, adaptive stepping at maxCo=0.2 and a final time of 1.5 with outputs every 0.15. Run one branch continuously from t=0 to 1.5. Run a second branch from t=0 to 0.75, write a complete binary restart state, and continue from the latest saved time to t=1.5 without reinitializing the fields. Compare the final rho, p, T and U fields, both centre-line profiles, time-step histories and output-time alignment between the continuous and restarted runs.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/2", "track": "extended", "case_id": "riemann2D/2", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a spatial-convergence study of the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use the square domain [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov central-upwind flux, vanAlbada reconstruction for rho and T, and vanAlbadaV reconstruction for U. Use zero-gradient conditions on the four outer sides and empty front/back patches. Advance to t=1.5 with adaptive time stepping and maxCo=0.2, writing results every 0.15 time units. Run otherwise identical uniform 200 x 200, 400 x 400 and 800 x 800 meshes, with outputs at the same physical times. Compare the density and pressure fields and centre-line profiles across the three resolutions, and discuss the observed convergence behaviour in smooth regions and across shocks and contact discontinuities.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/3", "track": "extended", "case_id": "riemann2D/3", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Assess Courant-number sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a fixed uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use the Kurganov flux with vanAlbada reconstruction for rho and T and vanAlbadaV for U, with zero-gradient outer boundaries. Run otherwise identical adaptive-time-step branches with maxCo=0.1 and maxCo=0.2 to t=1.5, writing both at the same physical times every 0.15. Compare their density and pressure fields, centre-line profiles, wave positions and computational effort.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/4", "track": "extended", "case_id": "riemann2D/4", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Compare the Kurganov and Tadmor central fluxes for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use vanAlbada reconstruction for rho and T and vanAlbadaV for U, zero-gradient outer boundaries, adaptive stepping with maxCo=0.2, and run to t=1.5 with outputs every 0.15. Change only the flux formulation between the two branches, and compare their density and pressure fields, centre-line profiles, discontinuity resolution, numerical oscillations, robustness and computational cost.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/5", "track": "extended", "case_id": "riemann2D/5", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Assess reconstruction-limiter sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Retain the Kurganov flux, zero-gradient outer boundaries, adaptive stepping with maxCo=0.2 and an end time of 1.5 with outputs every 0.15. Compare a vanAlbada/vanAlbadaV branch against a vanLeer/vanLeerV branch, changing only the reconstruction limiter. Compare density and pressure fields and centre-line profiles, with attention to discontinuity sharpness, post-shock oscillations and robustness.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/6", "track": "extended", "case_id": "riemann2D/6", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Evaluate mesh-orientation bias for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 Cartesian mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Run a baseline branch and a second branch in which the initial discontinuity geometry is rotated by 45 degrees while the mesh remains fixed. Define x'=(x+y)/sqrt(2) and y'=(-x+y)/sqrt(2), assign the same four states according to the signs of x' and y', and rotate their velocity vectors consistently into the physical x-y frame. Use the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries and maxCo=0.2, and run both branches to t=1.5 with outputs every 0.15. Rotate the second result back to the baseline frame and compare the density and pressure fields on the common interior [-3.5,3.5] x [-3.5,3.5].", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/7", "track": "extended", "case_id": "riemann2D/7", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Assess domain-size and outer-boundary sensitivity for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use one cell through the empty direction in both domains. Use the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries and maxCo=0.2. Run a small domain [-2.5,2.5] x [-2.5,2.5] on a 300 x 300 mesh and a large domain [-5,5] x [-5,5] on a 600 x 600 mesh, so that both use the same spatial resolution. Advance both to t=1.5 and write at matched times every 0.15. Compare their flow fields on the common interior [-2,2] x [-2,2] and identify when and how the smaller outer boundary begins to affect the solution.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/8", "track": "extended", "case_id": "riemann2D/8", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Stress-test positivity and nonlinear robustness for a strengthened four-quadrant two-dimensional Riemann interaction using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Use a uniform 600 x 600 mesh on [-5,5] x [-5,5] with one cell through the empty direction. Initialize (rho,p,u,v) as NE=(1.5,3.0,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.069,0.0145,1.206,1.206), and SE=(0.5323,0.3,0,1.206), deriving temperature consistently from the equation of state. Use the Kurganov flux, vanAlbada reconstruction for rho and T, vanAlbadaV for U, zero-gradient outer boundaries and adaptive stepping with maxCo=0.2. Attempt to reach t=1.5 without clipping, flooring or changing the stated physics. If the calculation fails, retain the failing configuration and identify the first failure time and affected field.", "external_asset_ids": []}
+{"task_id": "extended:riemann2D/9", "track": "extended", "case_id": "riemann2D/9", "family": "riemann2D", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Evaluate parallel-decomposition invariance and solver scaling for the CFD-China four-quadrant two-dimensional Riemann problem using OpenFOAM-13 with foamRun -solver shockFluid. Model an inviscid calorically perfect gas with gamma=1.4 using molWeight=11640.3, Cp=2.5, hf=0, mu=0 and Pr=1. Initialize the primitive states (rho,p,u,v) as NE=(1.5,1.5,0,0), NW=(0.5323,0.3,1.206,0), SW=(0.138,0.029,1.206,1.206), and SE=(0.5323,0.3,0,1.206), and derive temperature from the perfect-gas equation of state. Use a uniform 800 x 800 mesh over [-5,5] x [-5,5] with one cell through the empty direction, the Kurganov flux, vanAlbada/vanAlbadaV reconstruction, zero-gradient outer boundaries, maxCo=0.2 and an end time of 1.5 with outputs every 0.15. Execute matched serial, two-rank and four-rank runs, using scotch decomposition for the parallel branches. Compare the reconstructed final fields and centre-line profiles and report speedup and parallel efficiency. Measure elapsed time for the foamRun solver phase only, excluding mesh generation, initialization, decomposition, reconstruction, sampling and comparison.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/1", "track": "extended", "case_id": "risingBubble/1", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/10", "track": "extended", "case_id": "risingBubble/10", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=6.125, water density=1000 kg/m3, air density=100 kg/m3, liquid kinematic viscosity nu=0.1, air kinematic viscosity nu=0.1, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. This is a high-Eotvos-number and high-Morton-number sensitivity variant using lower surface tension and higher viscosity than the baseline, intended to explore a strongly deformed/skirt-bubble regime. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.1 and 0.1 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/2", "track": "extended", "case_id": "risingBubble/2", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 40x80 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/3", "track": "extended", "case_id": "risingBubble/3", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 80x160 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/4", "track": "extended", "case_id": "risingBubble/4", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Change only the interface-capturing scheme relative to the vanLeer baseline: use the explicit interfaceCompression alpha-transport scheme with a linear base interpolation instead of the baseline Gauss vanLeer alpha advection. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/5", "track": "extended", "case_id": "risingBubble/5", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. This variant follows the PDF design intent of an isoAdvector geometric reconstruction comparison, but OpenFOAM Foundation v13 does not provide the original isoAdvector method in this solver path; implement the closest available geometric VOF analogue as Gauss PLIC interfaceCompression vanLeer 1. Therefore the research purpose is comparable to the isoAdvector variant, while the numerical method entity is the Foundation-v13 PLIC/interfaceCompression approximation rather than native isoAdvector. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/6", "track": "extended", "case_id": "risingBubble/6", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=12.25, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/7", "track": "extended", "case_id": "risingBubble/7", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=49.0, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/8", "track": "extended", "case_id": "risingBubble/8", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=24.5, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. Use adaptive mesh refinement with dynamicRefineFvMesh to refine the mesh around the gas-liquid interface during the calculation, while keeping the initial coarse mesh and baseline physical properties; implement the reference case as a thin quasi-2D slab with front/back symmetry planes if needed for OpenFOAM dynamic refinement. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:risingBubble/9", "track": "extended", "case_id": "risingBubble/9", "family": "risingBubble", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a 2D rising-bubble VOF validation case using OpenFOAM-13 with foamRun -solver incompressibleVoF, corresponding to the legacy interFoam application. Use a rectangular domain discretized with 20x40 cells; initialize a circular gas bubble of radius 0.15 centered at (0.5, 0.8) in liquid. Set sigma=6.125, water density=1000 kg/m3, air density=100 kg/m3, and downward gravity=0.98 m/s2. Use the baseline vanLeer VOF alpha-advection scheme without the explicit interfaceCompression scheme variant. This is the high-Eotvos-number variant, using the lower surface tension as a physically consistent high-Eo parameter set so the bubble deforms more strongly than the baseline rising-bubble case. Run from t=0 to t=7; deltaT=1e-3; write results every 0.1 using writeControl=adjustableRunTime. Use adjustTimeStep=yes, maxCo=0.5, maxAlphaCo=0.9, maxDeltaT=0.9. Use a 1 m wide and 2 m high tank, initially at rest. Treat the side and bottom boundaries as slip walls and the top as an open pressure boundary. The flow is laminar; the water and air kinematic viscosities are 0.01 and 0.01 m2/s, respectively.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/1", "track": "extended", "case_id": "supersonicCrossJet/1", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: baseline Ma=2.0 and reference pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/10", "track": "extended", "case_id": "supersonicCrossJet/10", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the rhoPimpleFoam-style pseudo-transient solver switch in OpenFOAM-13 via foamRun -solver fluid. Variant: rhoPimpleFoam pseudo-transient solver-family switch relative to the rhoSimpleFoam steady baseline. Keep the Ma=2 physical geometry and inlet states of the baseline. Run a non-smoke transient PIMPLE window from t=0 to t=0.05 with deltaT=2e-6 and write every 0.005 simulation-time units. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/2", "track": "extended", "case_id": "supersonicCrossJet/2", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: mainflow Mach number Ma=3.0. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(1203 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/3", "track": "extended", "case_id": "supersonicCrossJet/3", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: low jet-to-mainstream pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=50000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/4", "track": "extended", "case_id": "supersonicCrossJet/4", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: high jet-to-mainstream pressure ratio. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=200000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/5", "track": "extended", "case_id": "supersonicCrossJet/5", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: 30 degree injection angle. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(300.749 173.637 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/6", "track": "extended", "case_id": "supersonicCrossJet/6", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: 60 degree injection angle. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(173.637 300.749 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/7", "track": "extended", "case_id": "supersonicCrossJet/7", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the compressible supersonic jet-in-crossflow benchmark with the same Ma=2, pressure ratio, thermophysical model, solver, and controls as the baseline, but refine the first active mainflow block in the streamwise direction from 40 to 80 cells. Preserve all other blocks, boundaries, and numerical schemes. This is the mesh-resolution variant; the 90-degree injection angle is already represented by the baseline case. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/8", "track": "extended", "case_id": "supersonicCrossJet/8", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: unbounded Gauss upwind convection retained for the full steady run, distinct from the bounded-upwind baseline. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:supersonicCrossJet/9", "track": "extended", "case_id": "supersonicCrossJet/9", "family": "supersonicCrossJet", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a compressible supersonic jet-in-crossflow benchmark using the legacy rhoSimpleFoam steady SIMPLE solver in OpenFOAM-13. Variant: earlier transition from upwind to bounded limitedLinear 0.05 steady schemes. Keep the physical geometry and inlet states unchanged except for the variant named here. This is a non-smoke steady benchmark: run steady iterations with deltaT=1 to endTime=1000 and write every 250 iterations. Judge success by solver stability, residual/continuity history, and final-window field changes rather than by a single iteration. For this staged scheme variant, run system/fvSchemes.upwind from iteration 0 to 300, then continue from latestTime with system/fvSchemes.limitedLinear, using bounded limitedLinear 0.05 convection, to iteration 1000. Use a quasi-2D channel extending from x=-3.33333 to 2 m with a height of 1 m. A 0.05 m wide jet slot lies in the lower wall immediately upstream of x=0; the remaining solid boundaries are slip walls and the right boundary is an extrapolating outlet. Set the main-stream state to U=(801.997 0 0) m/s, p=100000 Pa and T=400 K, and the jet state to U=(0 347.275 0) m/s, p=100000 Pa and T=300 K. Model laminar calorically perfect air with molecular weight 28.96, Cp=1004.5 J/(kg K), constant viscosity 1e-5 Pa s and Pr=1.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/1", "track": "extended", "case_id": "yPlusVerification/1", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 15 wall-normal cells with a grading ratio of 1 and the RAS kOmega turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/10", "track": "extended", "case_id": "yPlusVerification/10", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification viscosity-sensitivity comparison in a periodic half-channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, steady SIMPLE coupling, a 30-cell wall-normal mesh with grading ratio 50, and RAS kEpsilon. Run three nominal branches labelled Re_tau_180, Re_tau_395, and Re_tau_590 using nu=0.005555555556, 0.002531645570, and 0.001694915254 respectively while keeping meanVelocityForce Ubar=(0.4 0 0), geometry, boundaries, and controls fixed. The labels identify the viscosity values obtained from an initial u_tau=1 estimate; do not assume they are achieved Reynolds numbers. For every converged branch, obtain u_tau from positive computed wall shear, calculate and report achieved Re_tau=u_tau*delta/nu with delta=1, and compare sampled u+ versus y+ against Spalding law. Fail post-processing if wall shear is unavailable. The half-channel height is 1 m; the nominal Reynolds-number labels are only branch names, and the achieved friction Reynolds number must come from the computed wall shear.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/2", "track": "extended", "case_id": "yPlusVerification/2", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 15 wall-normal cells with a grading ratio of 1 and the RAS kEpsilon turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/3", "track": "extended", "case_id": "yPlusVerification/3", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LaunderSharmaKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/4", "track": "extended", "case_id": "yPlusVerification/4", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LamBremhorstKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/5", "track": "extended", "case_id": "yPlusVerification/5", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS LienCubicKE low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/6", "track": "extended", "case_id": "yPlusVerification/6", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS v2f low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/7", "track": "extended", "case_id": "yPlusVerification/7", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a wall y+ verification in a 1D periodic turbulent channel using OpenFOAM-13 with foamRun -solver incompressibleFluid, corresponding to the legacy simpleFoam application with steady-state SIMPLE pressure-velocity coupling. Use cyclic streamwise boundaries, a no-slip wall, a symmetry-plane centreline, and an empty front/back direction. Use 50 wall-normal cells with a grading ratio of 100 and the RAS qZeta low-Reynolds-number turbulence model. Use kinematic viscosity nu=2e-5 and drive the flow with meanVelocityForce Ubar=(0.4 0 0) on the fluid cellZone. Run steady-state SIMPLE iterations using startTime=0, endTime=2500, deltaT=0.25, writeControl=runTime, and writeInterval=100 as the iteration and output controls. Compare the sampled u+ versus y+ wall-law profile against the Spalding law analytical profile. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/8", "track": "extended", "case_id": "yPlusVerification/8", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform a steady wall y+ verification in the same 1D periodic channel as yPlusVerification/1 and /2, using foamRun -solver incompressibleFluid, SIMPLE coupling, RAS kOmegaSST, 15 wall-normal cells, uniform grading, nu=2e-5, meanVelocityForce Ubar=(0.4 0 0), endTime=500, deltaT=0.25, writeControl=runTime, and writeInterval=20. This is the third-model comparison against the kOmega and kEpsilon variants. Take the half-channel height as 1 m.", "external_asset_ids": []}
+{"task_id": "extended:yPlusVerification/9", "track": "extended", "case_id": "yPlusVerification/9", "family": "yPlusVerification", "task_origin": "ExtFoamBench (EasyFoam authors)", "usr_requirement": "Perform the coarse-wall-resolution y+ verification variant with the standard RAS kOmega model on the 30-cell wall-normal mesh with simpleGrading ratio 50. Keep the periodic channel forcing, endTime=500, deltaT=0.25, sampling, and Spalding comparison workflow fixed; this is distinct from the 15-cell kOmega baseline because the mesh and resulting wall-resolution target differ. Take the half-channel height as 1 m. Use kinematic viscosity 2e-5 m2/s and target mean velocity 0.4 m/s.", "external_asset_ids": []}
diff --git a/docs/DATA_FORMAT.md b/docs/DATA_FORMAT.md
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+# Data format and relationships
+
+The Hub table is a lossless projection of each source task's `usr_requirement`, with metadata added. It does not replace the original benchmark JSON documents.
+
+| Table field | Type | Meaning |
+| --- | --- | --- |
+| `task_id` | string | Unique across tracks: `<track>:<case_id>` |
+| `track` | string | `extended`, `basic`, or `advanced` |
+| `case_id` | string | Original source identifier; Advanced IDs need not contain `/` |
+| `family` | string | Source ID prefix before `/`, or the complete unsuffixed ID |
+| `task_origin` | string | Original ExtFoamBench task versus inherited/adapted FoamBench task |
+| `usr_requirement` | string | Original natural-language requirement, unchanged |
+| `external_asset_ids` | list of strings | Keys in `benchmarks/assets/manifest.json` |
+
+## Joining tasks to evaluation data
+
+Use `(track, case_id)` as the key. The evaluator profile at `benchmarks/evaluation/profiles/<track>.json` points to the exact benchmark and reference-QoI JSON files. The original case documents are dictionaries keyed by `case_id`. The reference-QoI documents and numerical-statistics documents contain a `cases` dictionary keyed by that same identifier.
+
+Reference case records include file contents under keys such as `0/U`, `system/controlDict`, and `Allrun`. Extended records may also have `_external_assets` and `reference_subcases`. These are reference configurations and must not be exposed to the solving agent as task input.
+
+Reference-QoI records preserve `principal_metrics`, `qois`, `tolerances`, and additional track-specific metadata. Scalar, profile, history, event and branch structures stay in their original JSON representation; converting them into one flat scalar column would lose evaluation semantics.
+
+Extended measurement definitions are in the `cases` mapping of `FoamBench_extended_openfoam13_measurement_specs.json`. These contain measurement definitions rather than numerical reference answers. Family-level design is in the `families` list of `FoamBench_extended_openfoam13_qoi_design.json`.
+
+Numerical diagnostics are in `benchmarks/reference_statistics/<track>.json`. An empty object denotes unavailable reference statistics. Do not equate it with zero residual, a passing check, or a missing reference-QoI record. Historical `log_paths` identify provenance; the named raw logs are not distributed.
+
+## Hugging Face configurations
+
+`extended` (default, 100 tasks), `basic` (110), `advanced` (16), and `all` (226) each expose one `test` split. These configurations distinguish task provenance and evaluation tracks. They are not training splits or the historical construction/validation/held-out split for skill evolution.
+
+The complete package retains legacy `FoamBench_extended_*` filenames for compatibility with the supplied scorer. On the dataset page, this track is named ExtFoamBench.
diff --git a/docs/EVALUATION.md b/docs/EVALUATION.md
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index 0000000000000000000000000000000000000000..f8fadbb17c3ac523a4b1d5749ee5be37154003df
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+++ b/docs/EVALUATION.md
@@ -0,0 +1,49 @@
+# Evaluation protocol and executable scorer
+
+The EasyFoam authors developed the evaluation framework and generated the offline reference data for all three tracks. Basic and Advanced task definitions remain credited to upstream FoamBench.
+
+## Metrics and output fields
+
+| Concept | Report field under `overall` | Denominator |
+| --- | --- | --- |
+| ECR | `execution_pass_rate` | Complete assigned profile membership |
+| Numerical acceptance | `numerical_pass_rate_all_tasks` | Complete assigned profile membership |
+| Physical/QoI acceptance | `physics_grounded_qoi_pass_rate_all_tasks` | Complete assigned profile membership |
+| TAR / joint acceptance | `end_to_end_pass_rate` | Complete assigned profile membership |
+
+Execution must pass before Numerical/QoI task acceptance is credited. All mandatory physical metrics must pass; a continuous quality score cannot override a failed mandatory metric. Missing rollouts remain in the denominator. Conditional-on-execution rates are separately reported. Full-profile evaluation of a one-task run counts the other tasks as missing; inspect the case-level result when testing one task.
+
+## Evaluate existing artifacts
+
+From the repository root, after installing `requirements.txt`:
+
+```bash
+python -m benchmarks.evaluation evaluate --profile benchmarks/evaluation/profiles/extended.json --adapter easyfoam --run-root /path/to/existing/run --output outputs/evaluation
+```
+
+`/path/to/existing/run` is user-supplied data, not a bundled example. The adapters are `easyfoam`, `foamagent`, `chatcfd`, and `coding-agent`; they normalize different retained-run layouts. Adapter selection alone does not make an arbitrary folder compatible: consult `benchmarks/evaluation/adapters/` for required artifacts. No agent runtime or model call is performed by this command.
+
+Outputs include `campaign_evaluation.json`, `summary.json`, `summary.csv`, `cases.csv`, and per-case JSON reports. ECR and TAR are fractions from 0 to 1; multiply by 100 for percentages.
+
+## QoI and numerical evidence
+
+The supplied Extended design specifies principal versus diagnostic quantities and task branches. Measurement specs define the physical quantity, spatial support, and time semantics; the reference records supply comparison values and tolerances. Structured comparison preserves curves, events and branch-dependent responses, rather than replacing them with generic field extrema.
+
+Numerical checks use retained logs/fields and applicable reference statistics. Missing reference statistics are explicitly recorded. The evidence contract supports a validated manifest, retained-field derivation, semantic path discovery, and unresolved-evidence reporting. A filename match alone does not establish units, physical support, or time alignment.
+
+## Native tools and preparation
+
+Most offline checks use Python and retained outputs. Static planar-face meshes can supply cell centers/volumes directly. Some geometry or topology-changing histories require native OpenFOAM measurement tools. In particular, the supplied extractor may invoke `foamPostProcess` for missing time-local `C/Vc` fields; offline evaluation is not an unconditional read-only/no-OpenFOAM guarantee.
+
+Use copies of valuable retained runs when derived fields may be generated. `--prepare` explicitly prepares measurement fields and writes preparation logs. `--check-mesh` enables a fresh mesh audit when required. These options do not rerun the CFD agent. Actual OpenFOAM tool execution was not verified on Windows during dataset packaging.
+
+## Current implementation boundaries
+
+- Extended reference tolerances retain `joint_physical_admissibility_and_reference_response_provisional`. This release does not silently upgrade them to calibrated uncertainty bounds.
+- The supplied Basic/Advanced scorer describes mandatory physical ranges/signatures, with structured profiles/histories/shock locations retained as reference-agreement diagnostics. The paper also describes profile acceptance criteria. Exact manuscript-to-implementation alignment must be checked before claiming identical historical scores.
+- Spatial profile coverage counts profile-field combinations rather than individual reference sampling points.
+- Early-convergence markers can satisfy the execution stop condition.
+- Historical scalar-QoI and older numerical-contract results are not automatically comparable to this version.
+- Historical agent outputs and paper result archives are absent. This release enables reuse of the supplied benchmark/evaluator and does not itself replay the manuscript tables.
+
+When comparing systems, freeze the same task membership, reference records, scorer version, and acceptance rules for every method. Changing these defines a different evaluation protocol.
diff --git a/docs/PROVENANCE.md b/docs/PROVENANCE.md
new file mode 100644
index 0000000000000000000000000000000000000000..9baad0a99452971113e8ebf63913ee16a789c0e6
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+++ b/docs/PROVENANCE.md
@@ -0,0 +1,29 @@
+# Contribution attribution and provenance
+
+## Original EasyFoam contributions
+
+- **ExtFoamBench task design:** 100 tasks in ten families, with task variants covering physical settings and workflows.
+- **Evaluation resources:** execution/numerical/physical acceptance framework, TAR reporting, task-specific QoI measurement and acceptance specifications, evidence contracts, and the supplied evaluation implementation.
+- **Offline reference data:** reference simulations and derived QoI/numerical-statistics records generated by the EasyFoam authors for **Extended, Basic, and Advanced**.
+
+Original task design does not imply that every geometry, tutorial input, physical problem, or underlying simulation tool was created from scratch.
+
+## Inherited task definitions
+
+The **110 Basic and 16 Advanced tasks** originate from FoamBench / CFDLLMBench. They are redistributed here as OpenFOAM Foundation 13 adaptations to support the new evaluation and reference-data resources. They are not claimed as original EasyFoam tasks.
+
+Upstream: https://github.com/NLR-Theseus/cfdllmbench (the former NREL-Theseus URL redirects here).
+
+The upstream BSD-3-Clause notice is retained at `LICENSES/FoamBench-BSD-3-Clause.txt`. Cite the upstream work when using these tracks, in addition to EasyFoam when using its evaluator or offline reference data.
+
+## CFD sources and geometry
+
+The EasyFoam paper's Appendix A describes source cases including dyfluid tutorials, OpenFOAM tutorial geometries, and CFD-China material, with additional physical references. Consult the paper for family-level scientific attribution; this release does not invent more precise upstream revisions than the supplied source records establish.
+
+Seven OpenFOAM 13 geometry assets are accompanied by their original tutorial locations and SHA-256 digests in `benchmarks/assets/manifest.json`. The original asset README and GPL text are retained. Existing third-party notices within case text remain unchanged. DrivAer is an existing geometry, not an original EasyFoam geometry.
+
+## Snapshot and transformation
+
+`metadata/source_manifest.json` identifies the original files copied from the supplied research snapshot, with byte hashes. The HF release does not modify their contents, scoring code, reference values or tolerances. It adds task tables, documentation, inspection/verification utilities, and release metadata. Its evaluator README is tailored to this standalone distribution; agent campaign/evolution launchers are not bundled.
+
+The JSONL tables are deterministic projections of the original task requirements, with track/origin metadata and asset identifiers. `metadata/coverage.json` records reference-data availability. Raw simulation provenance cannot be reconstructed solely from compact reference summaries; raw logs and solution fields are not present in this package.
diff --git a/docs/RELEASE_NOTES.md b/docs/RELEASE_NOTES.md
new file mode 100644
index 0000000000000000000000000000000000000000..f8b1b8ee13a4d283c307afca38eee81d388c7f8d
--- /dev/null
+++ b/docs/RELEASE_NOTES.md
@@ -0,0 +1,27 @@
+# Release 1.0.0
+
+Prepared on 2026-10-12 from the supplied EasyFoam research snapshot.
+
+## Included
+
+- 100 original ExtFoamBench tasks as the default Hub configuration.
+- 110 inherited Basic and 16 inherited Advanced tasks, separately attributed.
+- EasyFoam evaluation/reference resources for all 226 tasks.
+- Unmodified source JSON, geometry assets, evaluation Python files, and required schemas.
+- Hub-readable task tables, standalone documentation, inspection/verification commands, source hashes and coverage metadata.
+
+## Coverage and limits
+
+All tracks have matching task/reference-QoI case membership. Numerical reference statistics are empty for `nozzleCDV/4` and all ten `riemann2D` tasks (11 total). Conditional or diagnostic availability should be read from individual records, not inferred from case counts.
+
+Raw solution fields/logs, historical agent rollouts, Initial/Evolved checkpoints, historical evolution split manifests, and paper-result archives are outside this release. The reference-repeat/physical-negative-control and tolerance-sensitivity experiments described in the paper are not supplied here as independent raw result archives.
+
+Embedded protocol statuses, including provisional Extended tolerances, are preserved. The release version identifies a packaged snapshot; it is not a certification of exact historical manuscript reproduction. See `EVALUATION.md` for protocol boundaries.
+
+## Validation
+
+See `metadata/validation.json` for checks executed during packaging and `SHA256SUMS` for file integrity. These checks concern data consistency, loading and offline software behavior, not a new CFD reference rerun or a model benchmark campaign.
+
+## Updating
+
+If tasks, references, measurement definitions or scorer behavior change, publish a new version and describe the change. Keep a tag/revision identifying each evaluated release. Updating display text alone must not silently replace scientific data associated with a reported result.
diff --git a/examples/inspect_task.py b/examples/inspect_task.py
new file mode 100644
index 0000000000000000000000000000000000000000..a1672cc97e601402255bd68c776cad40dfa27976
--- /dev/null
+++ b/examples/inspect_task.py
@@ -0,0 +1,22 @@
+"""Inspect a task and evaluator-side reference summary without third-party dependencies."""
+import argparse
+import json
+from pathlib import Path
+ROOT = Path(__file__).resolve().parents[1]
+def main():
+    parser = argparse.ArgumentParser(description=__doc__)
+    parser.add_argument('--track', choices=('extended','basic','advanced'), default='extended')
+    parser.add_argument('--case-id', default='nozzleCDV/1')
+    args = parser.parse_args()
+    rows = [json.loads(line) for line in (ROOT/f'data/{args.track}.jsonl').read_text(encoding='utf-8').splitlines()]
+    row = next((x for x in rows if x['case_id']==args.case_id),None)
+    if row is None: parser.error(f'Unknown case {args.case_id!r} for {args.track}')
+    profile = json.loads((ROOT/f'benchmarks/evaluation/profiles/{args.track}.json').read_text(encoding='utf-8'))
+    refs = json.loads((ROOT/profile['reference_qois_path']).read_text(encoding='utf-8'))['cases']
+    stats = json.loads((ROOT/f'benchmarks/reference_statistics/{args.track}.json').read_text(encoding='utf-8'))['cases']
+    result = {'task':row,'reference_metric_names':refs[args.case_id].get('principal_metrics',[]),'reference_qoi_file':profile['reference_qois_path'],'reference_case_file':profile['benchmark_path'],'numerical_reference_statistics_available':bool(stats[args.case_id])}
+    if args.track=='extended':
+        specs=json.loads((ROOT/'benchmarks/FoamBench_extended_openfoam13_measurement_specs.json').read_text(encoding='utf-8'))
+        result['measurement_spec']=specs['cases'][args.case_id]
+    print(json.dumps(result,indent=2,ensure_ascii=True))
+if __name__=='__main__': main()
diff --git a/metadata/coverage.json b/metadata/coverage.json
new file mode 100644
index 0000000000000000000000000000000000000000..a4d4231ff2f0c4bc2096f23172761883588660a7
--- /dev/null
+++ b/metadata/coverage.json
@@ -0,0 +1,38 @@
+{
+  "extended": {
+    "task_count": 100,
+    "reference_qoi_case_entries": 100,
+    "nonempty_numerical_statistics_entries": 89,
+    "missing_numerical_statistics_case_ids": [
+      "nozzleCDV/4",
+      "riemann2D/1",
+      "riemann2D/10",
+      "riemann2D/2",
+      "riemann2D/3",
+      "riemann2D/4",
+      "riemann2D/5",
+      "riemann2D/6",
+      "riemann2D/7",
+      "riemann2D/8",
+      "riemann2D/9"
+    ],
+    "original_task_contribution": true,
+    "evaluation_and_offline_reference_data_contributor": "EasyFoam authors"
+  },
+  "basic": {
+    "task_count": 110,
+    "reference_qoi_case_entries": 110,
+    "nonempty_numerical_statistics_entries": 110,
+    "missing_numerical_statistics_case_ids": [],
+    "original_task_contribution": false,
+    "evaluation_and_offline_reference_data_contributor": "EasyFoam authors"
+  },
+  "advanced": {
+    "task_count": 16,
+    "reference_qoi_case_entries": 16,
+    "nonempty_numerical_statistics_entries": 16,
+    "missing_numerical_statistics_case_ids": [],
+    "original_task_contribution": false,
+    "evaluation_and_offline_reference_data_contributor": "EasyFoam authors"
+  }
+}
diff --git a/metadata/families.json b/metadata/families.json
new file mode 100644
index 0000000000000000000000000000000000000000..b4bb2725a57c307ac7d52f2408131d0c0762d064
--- /dev/null
+++ b/metadata/families.json
@@ -0,0 +1,187 @@
+[
+  {
+    "track": "extended",
+    "family": "ERCOFTA_pump",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "MRF_stirredReactor",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "aerofoilNACA0012",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "compressibleBubbleCollapse",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "drivaerFastback",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "nozzleCDV",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "riemann2D",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "risingBubble",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "supersonicCrossJet",
+    "task_count": 10
+  },
+  {
+    "track": "extended",
+    "family": "yPlusVerification",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "BernardCells",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "Cavity",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "Cylinder",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "counterFlowFlame2D",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "damBreakWithObstacle",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "forwardStep",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "obliqueShock",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "pitzDaily",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "shallowWaterWithSquareBump",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "squareBend",
+    "task_count": 10
+  },
+  {
+    "track": "basic",
+    "family": "wedge",
+    "task_count": 10
+  },
+  {
+    "track": "advanced",
+    "family": "Cavity_LES",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Cavity_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Cavity_geometry_1",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Cylinder_LES",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Cylinder_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Diamond_Obstacle_KOMEGASST",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Diamond_Obstacle_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Double_Square_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Rectangular_Obstacle_KOMEGASST",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "Rectangular_Obstacle_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "counterFlowFlame2D_KE",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "counterFlowFlame2D_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "nozzleFlow2D_SA",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "obliqueShock_KE",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "obliqueShock_LES",
+    "task_count": 1
+  },
+  {
+    "track": "advanced",
+    "family": "wedge_SA",
+    "task_count": 1
+  }
+]
diff --git a/metadata/release.json b/metadata/release.json
new file mode 100644
index 0000000000000000000000000000000000000000..e314f57ca437dfd14cee90d6fc6f7421efb22545
--- /dev/null
+++ b/metadata/release.json
@@ -0,0 +1,18 @@
+{
+  "release_version": "1.0.0",
+  "release_date": "2026-10-12",
+  "dataset_name": "ExtFoamBench",
+  "new_task_count": 100,
+  "inherited_task_count": 126,
+  "evaluation_task_count": 226,
+  "default_hf_config": "extended",
+  "hf_split": "test",
+  "split_meaning": "Benchmark tasks; not the historical evolution held-out split",
+  "openfoam_distribution": "OpenFOAM Foundation 13",
+  "paper_url": "https://openreview.net/forum?id=GhQ5YmhU8B",
+  "code_url": "https://github.com/CAS-CLab/EasyFoam",
+  "protocol_status": "Frozen supplied implementation; preserve embedded contract versions and provisional tolerance status",
+  "historical_paper_result_reproduction_certified": false,
+  "huggingface_repo_id": "Eurus132/ExtFoamBench",
+  "huggingface_url": "https://huggingface.co/datasets/Eurus132/ExtFoamBench"
+}
diff --git a/metadata/source_manifest.json b/metadata/source_manifest.json
new file mode 100644
index 0000000000000000000000000000000000000000..378f33d7409ed1995d720e48f49554523abadcb3
--- /dev/null
+++ b/metadata/source_manifest.json
@@ -0,0 +1,418 @@
+{
+  "schema_version": "extfoambench.source-manifest.v1",
+  "source_description": "User-supplied EasyFoam research source snapshot",
+  "copied_files_byte_identical": true,
+  "files": [
+    {
+      "path": "benchmarks/__init__.py",
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+    },
+    {
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+    {
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+      "bytes": 24058
+    },
+    {
+      "path": "benchmarks/evaluation/reference.py",
+      "sha256": "627725f472e89d9b97ff8cedf23d2ac92097a53f27f23d648f7be0bf943d33b1",
+      "bytes": 1684
+    },
+    {
+      "path": "benchmarks/evaluation/reporting.py",
+      "sha256": "159655e9dadb4367a59a7ea1a804856c5280b3bc025c2892f06fd0535e265bae",
+      "bytes": 3765
+    },
+    {
+      "path": "benchmarks/evaluation/retained_fields.py",
+      "sha256": "0c54e9671b9f7353cbc28ecf9798d678db4bfacaa5f7c184bf4e45ebef9ec4a7",
+      "bytes": 14447
+    },
+    {
+      "path": "benchmarks/evaluation/schema.py",
+      "sha256": "477332e61a0f668ff51db9817ec874706051d37c2dedf65b5ca43b73435c9583",
+      "bytes": 731
+    },
+    {
+      "path": "benchmarks/evaluation/stability.py",
+      "sha256": "b9ba1b4c4583e9b393c699d47bab71a82aed159519408062b631147bd70d25a5",
+      "bytes": 1878
+    },
+    {
+      "path": "benchmarks/FoamBench_advanced_openfoam13_fixed_final.json",
+      "sha256": "74133664f968335b38cd17a0265d5003a4cce52230fc3f03846fcd3315599027",
+      "bytes": 306717
+    },
+    {
+      "path": "benchmarks/FoamBench_advanced_openfoam13_reference_qois.json",
+      "sha256": "31f46baabdbfb1482d8ef2573d25b82cd1c40f6859bf71cddae6f12e80fbba63",
+      "bytes": 357142
+    },
+    {
+      "path": "benchmarks/FoamBench_basic_openfoam13_fixed_final.json",
+      "sha256": "50588c363869dd0a37befaa8e91bbc83c7bd8b14d8a23ff1eb2dc66fd77a0523",
+      "bytes": 2026359
+    },
+    {
+      "path": "benchmarks/FoamBench_basic_openfoam13_reference_qois.json",
+      "sha256": "6f91688f7c97b3ef6b8191256c14af7f8accb168e8d384aba763681e01c34724",
+      "bytes": 2031952
+    },
+    {
+      "path": "benchmarks/FoamBench_extended_openfoam13_evidence_contract.v1.json",
+      "sha256": "4f0eae169c7d575da991d7c23c313ce6e4971887fbbaffbbbf9bc65105c2b676",
+      "bytes": 2985
+    },
+    {
+      "path": "benchmarks/FoamBench_extended_openfoam13_fixed.json",
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+      "bytes": 2260175
+    },
+    {
+      "path": "benchmarks/FoamBench_extended_openfoam13_measurement_specs.json",
+      "sha256": "0bddaf5b3abc3569d105c89cbdeef8cf3c4cce381ba9f7a3d622cadadaf8a68b",
+      "bytes": 148565
+    },
+    {
+      "path": "benchmarks/FoamBench_extended_openfoam13_qoi_design.json",
+      "sha256": "fb1db5034a1d2688ad360c6b0810bab68c33d4c6dc1dc5bec29095e93b077393",
+      "bytes": 20291
+    },
+    {
+      "path": "benchmarks/FoamBench_extended_openfoam13_reference_qois.json",
+      "sha256": "65e5c2d9968d1dbc798d585c9398c6fba2646f7463909040ae0c039727c8a1f9",
+      "bytes": 7742495
+    },
+    {
+      "path": "benchmarks/reference_statistics/advanced.json",
+      "sha256": "6c4a770c4b750ab0a8587cd18543517fd45cc93671014ced5fc81d668cd8a41b",
+      "bytes": 25631
+    },
+    {
+      "path": "benchmarks/reference_statistics/basic.json",
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+      "bytes": 148470
+    },
+    {
+      "path": "benchmarks/reference_statistics/extended.json",
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+      "bytes": 154741
+    },
+    {
+      "path": "benchmarks/scripts/__init__.py",
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+      "bytes": 87
+    },
+    {
+      "path": "benchmarks/scripts/build_extbench_reference.py",
+      "sha256": "113840a36b914722ff422505b1ed128daf023ee20bf287ab8ebfcd1af938a786",
+      "bytes": 7060
+    },
+    {
+      "path": "benchmarks/scripts/compare_foambench_qois.py",
+      "sha256": "827836c6f2363f0104917b6573dc86935ffc58fd3b9dcdf0ca83cd5ce874f753",
+      "bytes": 446
+    },
+    {
+      "path": "benchmarks/scripts/extract_extbench_qois.py",
+      "sha256": "845727247e81e82d75abb0e05b62d1bd15f9a7d8512533b749b8a20e1631f6a5",
+      "bytes": 446
+    },
+    {
+      "path": "benchmarks/scripts/extract_foambench_candidate_qois.py",
+      "sha256": "1110f0962468820146307099c463c1be8a25cbc5c3729fd7abc116d7fe06d27a",
+      "bytes": 2020
+    },
+    {
+      "path": "benchmarks/scripts/extract_foambench_qois.py",
+      "sha256": "cf3c18a0329ac576fc05e35ba2f70f95f0c1d6668a86fe6a65d8402de41a1abe",
+      "bytes": 457
+    },
+    {
+      "path": "benchmarks/scripts/materialize_benchmark.py",
+      "sha256": "265ac1ec1fcc347c82e9351a86305d6f7bafaf3bd8ff69075904ebaf285ed2bc",
+      "bytes": 10921
+    },
+    {
+      "path": "benchmarks/scripts/recover_extbench_qoi.py",
+      "sha256": "fc1268f130f4b0800b5a75346198e97896bd5e74b07ea3face5d0e4afa0d6d2c",
+      "bytes": 13206
+    },
+    {
+      "path": "benchmarks/scripts/validate_benchmark_assets.py",
+      "sha256": "ca2f885342099b4a06f425d971bee5edc24b199b596000e9997f8940b23770b4",
+      "bytes": 3335
+    },
+    {
+      "path": "LICENSE",
+      "sha256": "cfc7749b96f63bd31c3c42b5c471bf756814053e847c10f3eb003417bc523d30",
+      "bytes": 11358
+    },
+    {
+      "path": "LICENSES/GPL-3.txt",
+      "sha256": "8ceb4b9ee5adedde47b31e975c1d90c73ad27b6b165a1dcd80c7c545eb65b903",
+      "bytes": 35147
+    },
+    {
+      "path": "schemas/benchmark_evaluation.schema.json",
+      "sha256": "d49505bf35dffc763df91b13c8b5885e78b607af56d7aceba01e427c3fa19a6b",
+      "bytes": 4758
+    },
+    {
+      "path": "schemas/benchmark_profile.schema.json",
+      "sha256": "32a7f0865e9c851848fc775f9bde1125bd03749b4130d34fe95d5ffc62a700c0",
+      "bytes": 1478
+    },
+    {
+      "path": "schemas/foambench_qoi_candidate.schema.json",
+      "sha256": "88fb894b919323c0457f1cb4bf934f72320d644299185127c164579343606425",
+      "bytes": 944
+    },
+    {
+      "path": "schemas/foambench_qoi_comparison.schema.json",
+      "sha256": "9204923e5b93e333459ccfc43394137deaee1bf19d6f01beaf8ada664806d7e8",
+      "bytes": 1179
+    },
+    {
+      "path": "schemas/foambench_qoi_reference.schema.json",
+      "sha256": "2ef632eb4ed82ad78213de6ee4b18aa36558916a106cb258505493c95285ac68",
+      "bytes": 2327
+    },
+    {
+      "path": "schemas/qoi_recovery_plan.schema.json",
+      "sha256": "839a77fa504b7f13b2b6803c0ca2448df83418779cee2a2a5a5acdc18cd8760c",
+      "bytes": 881
+    }
+  ],
+  "additional_upstream_notice": {
+    "path": "LICENSES/FoamBench-BSD-3-Clause.txt",
+    "source_url": "https://raw.githubusercontent.com/NLR-Theseus/cfdllmbench/main/LICENSE",
+    "retrieved_date": "2026-10-12",
+    "sha256": "7e0a18d9201969787f5fc32b977318576c7d2942f2828e19fa212bde19706a22"
+  }
+}
diff --git a/metadata/validation.json b/metadata/validation.json
new file mode 100644
index 0000000000000000000000000000000000000000..e10449a77c455c3c91b30bce719f47ca760b5b56
--- /dev/null
+++ b/metadata/validation.json
@@ -0,0 +1,167 @@
+{
+  "status": "pass",
+  "date": "2026-10-12",
+  "environment": {
+    "python": "3.12.14",
+    "datasets": "5.1.0",
+    "huggingface_hub": "2.2.0",
+    "numpy": "2.5.4",
+    "jsonschema": "4.19.2"
+  },
+  "checks": [
+    {
+      "check": "hf_dataset_card_configs",
+      "status": "pass",
+      "detail": [
+        "extended",
+        "basic",
+        "advanced",
+        "all"
+      ]
+    },
+    {
+      "check": "hf_load_extended",
+      "status": "pass",
+      "detail": {
+        "rows": 100,
+        "columns": [
+          "task_id",
+          "track",
+          "case_id",
+          "family",
+          "task_origin",
+          "usr_requirement",
+          "external_asset_ids"
+        ]
+      }
+    },
+    {
+      "check": "hf_load_basic",
+      "status": "pass",
+      "detail": {
+        "rows": 110,
+        "columns": [
+          "task_id",
+          "track",
+          "case_id",
+          "family",
+          "task_origin",
+          "usr_requirement",
+          "external_asset_ids"
+        ]
+      }
+    },
+    {
+      "check": "hf_load_advanced",
+      "status": "pass",
+      "detail": {
+        "rows": 16,
+        "columns": [
+          "task_id",
+          "track",
+          "case_id",
+          "family",
+          "task_origin",
+          "usr_requirement",
+          "external_asset_ids"
+        ]
+      }
+    },
+    {
+      "check": "hf_load_all",
+      "status": "pass",
+      "detail": {
+        "rows": 226,
+        "columns": [
+          "task_id",
+          "track",
+          "case_id",
+          "family",
+          "task_origin",
+          "usr_requirement",
+          "external_asset_ids"
+        ]
+      }
+    },
+    {
+      "check": "profile_extended",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "materialize_extended",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "profile_basic",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "materialize_basic",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "profile_advanced",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "materialize_advanced",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "geometry",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "inspect_example",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "empty_run_evaluation",
+      "status": "pass",
+      "detail": "exit 0"
+    },
+    {
+      "check": "missing_rollouts_denominator",
+      "status": "pass",
+      "detail": {
+        "assigned": 100,
+        "execution_pass_rate": 0,
+        "end_to_end_pass_rate": 0
+      }
+    },
+    {
+      "check": "python_syntax",
+      "status": "pass",
+      "detail": 51
+    },
+    {
+      "check": "local_markdown_links",
+      "status": "pass",
+      "detail": "all resolve"
+    },
+    {
+      "check": "credential_pattern_scan",
+      "status": "pass",
+      "detail": "no matches for common token/private-key signatures; not an exhaustive security audit"
+    }
+  ],
+  "evaluator_environment": {
+    "python": "3.12.14",
+    "numpy": "1.26.4",
+    "jsonschema": "4.19.2"
+  },
+  "not_run": [
+    "HF hosted dataset viewer (not uploaded)",
+    "CFD solver/reference reruns",
+    "model or agent inference",
+    "historical manuscript-table reproduction"
+  ]
+}
diff --git a/requirements.txt b/requirements.txt
new file mode 100644
index 0000000000000000000000000000000000000000..f65d8caa95c4b03d8aef03790310780ccbddcbcb
--- /dev/null
+++ b/requirements.txt
@@ -0,0 +1,2 @@
+numpy==1.26.4
+jsonschema==4.19.2
diff --git a/schemas/benchmark_evaluation.schema.json b/schemas/benchmark_evaluation.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..899ae724892171ea9addbfc6a93bbfe5b4d41e7d
--- /dev/null
+++ b/schemas/benchmark_evaluation.schema.json
@@ -0,0 +1,126 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "benchmark_evaluation.schema.json",
+  "title": "FoamBench Campaign and Case Evaluation",
+  "type": "object",
+  "additionalProperties": false,
+  "required": [
+    "schema_version",
+    "generated_at",
+    "profile_id",
+    "dataset",
+    "adapter",
+    "run_root",
+    "reference_qois",
+    "definitions",
+    "overall",
+    "families",
+    "cases"
+  ],
+  "properties": {
+    "schema_version": {"const": "foambench.campaign_evaluation.v1"},
+    "generated_at": {"type": "string", "format": "date-time"},
+    "profile_id": {"type": "string", "minLength": 1},
+    "dataset": {"type": "string", "minLength": 1},
+    "adapter": {"enum": ["easyfoam", "foamagent", "chatcfd", "coding-agent"]},
+    "run_root": {"type": "string", "minLength": 1},
+    "reference_qois": {"type": "string", "minLength": 1},
+    "definitions": {"type": "object"},
+    "overall": {"$ref": "#/$defs/summary"},
+    "families": {"type": "object", "additionalProperties": {"$ref": "#/$defs/summary"}},
+    "cases": {"type": "object", "additionalProperties": {"$ref": "#/$defs/case"}}
+  },
+  "$defs": {
+    "summary": {
+      "type": "object",
+      "required": [
+        "task_count",
+        "execution_pass_count",
+        "execution_pass_rate",
+        "numerical_pass_count",
+        "numerical_pass_rate_all_tasks",
+        "physics_grounded_qoi_pass_count",
+        "physics_grounded_qoi_pass_rate_all_tasks",
+        "end_to_end_pass_count",
+        "end_to_end_pass_rate",
+        "failure_taxonomy"
+      ],
+      "properties": {
+        "task_count": {"type": "integer", "minimum": 0},
+        "execution_pass_count": {"type": "integer", "minimum": 0},
+        "execution_pass_rate": {"type": ["number", "null"], "minimum": 0, "maximum": 1},
+        "numerical_pass_count": {"type": "integer", "minimum": 0},
+        "numerical_pass_rate_all_tasks": {"type": ["number", "null"], "minimum": 0, "maximum": 1},
+        "physics_grounded_qoi_pass_count": {"type": "integer", "minimum": 0},
+        "physics_grounded_qoi_pass_rate_all_tasks": {"type": ["number", "null"], "minimum": 0, "maximum": 1},
+        "end_to_end_pass_count": {"type": "integer", "minimum": 0},
+        "end_to_end_pass_rate": {"type": ["number", "null"], "minimum": 0, "maximum": 1},
+        "failure_taxonomy": {"type": "object", "additionalProperties": {"type": "integer", "minimum": 0}}
+      }
+    },
+    "case": {
+      "type": "object",
+      "additionalProperties": true,
+      "required": [
+        "schema_version",
+        "case_id",
+        "dataset",
+        "family",
+        "variant",
+        "replicate",
+        "execution",
+        "numerical",
+        "qoi",
+        "scores",
+        "resources",
+        "artifact",
+        "failure_categories"
+      ],
+      "properties": {
+        "schema_version": {"const": "foambench.case_evaluation.v1"},
+        "case_id": {"type": "string", "minLength": 1},
+        "dataset": {"type": "string", "minLength": 1},
+        "family": {"type": "string", "minLength": 1},
+        "variant": {"type": "string", "minLength": 1},
+        "replicate": {"type": "integer", "minimum": 1},
+        "execution": {"$ref": "#/$defs/assessment"},
+        "numerical": {"$ref": "#/$defs/assessment"},
+        "qoi": {
+          "type": "object",
+          "required": ["status", "physics_grounded_qoi_pass", "effective_pass_ratio", "candidate"],
+          "properties": {
+            "status": {"type": "string"},
+            "physics_grounded_qoi_pass": {"type": "boolean"},
+            "effective_pass_ratio": {"type": "number", "minimum": 0, "maximum": 1},
+            "candidate": {"type": "object"},
+            "comparison": {"type": ["object", "null"]}
+          }
+        },
+        "scores": {
+          "type": "object",
+          "additionalProperties": false,
+          "required": ["execution_pass", "numerical_pass", "physics_grounded_qoi_pass", "end_to_end_pass"],
+          "properties": {
+            "execution_pass": {"type": "boolean"},
+            "numerical_pass": {"type": "boolean"},
+            "physics_grounded_qoi_pass": {"type": "boolean"},
+            "end_to_end_pass": {"type": "boolean"}
+          }
+        },
+        "resources": {"type": "object"},
+        "artifact": {"type": "object"},
+        "failure_categories": {"type": "array", "items": {"type": "string"}, "uniqueItems": true}
+      }
+    },
+    "assessment": {
+      "type": "object",
+      "required": ["schema_version", "status", "checks", "failed_checks"],
+      "properties": {
+        "schema_version": {"type": "string"},
+        "status": {"type": "string"},
+        "checks": {"type": "object"},
+        "failed_checks": {"type": "array", "items": {"type": "string"}}
+      }
+    }
+  }
+}
diff --git a/schemas/benchmark_profile.schema.json b/schemas/benchmark_profile.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..7438d9b4ed8a51fc969fc214171c15fd618964ed
--- /dev/null
+++ b/schemas/benchmark_profile.schema.json
@@ -0,0 +1,49 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "benchmark_profile.schema.json",
+  "title": "FoamBench Evaluation Profile",
+  "type": "object",
+  "additionalProperties": false,
+  "required": [
+    "profile_id",
+    "dataset",
+    "benchmark_path",
+    "reference_qois_path",
+    "membership",
+    "qoi",
+    "numerical"
+  ],
+  "properties": {
+    "profile_id": {"type": "string", "minLength": 1},
+    "dataset": {"type": "string", "minLength": 1},
+    "benchmark_path": {"type": "string", "minLength": 1},
+    "reference_qois_path": {"type": "string", "minLength": 1},
+    "reference_run_root": {"type": "string", "minLength": 1},
+    "membership": {
+      "type": "object",
+      "additionalProperties": false,
+      "required": ["expected_case_count", "case_id_style"],
+      "properties": {
+        "expected_case_count": {"type": "integer", "minimum": 1},
+        "case_id_style": {"enum": ["family_variant", "case_name"]}
+      }
+    },
+    "qoi": {
+      "type": "object",
+      "additionalProperties": false,
+      "required": ["extractor", "required_fraction"],
+      "properties": {
+        "extractor": {"enum": ["field", "extended"]},
+        "required_fraction": {"type": "number", "exclusiveMinimum": 0, "maximum": 1}
+      }
+    },
+    "numerical": {
+      "type": "object",
+      "additionalProperties": true,
+      "required": ["contract"],
+      "properties": {
+        "contract": {"type": "string", "minLength": 1}
+      }
+    }
+  }
+}
diff --git a/schemas/foambench_qoi_candidate.schema.json b/schemas/foambench_qoi_candidate.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..640f5af574379073ea44632a74fbe022f53a0010
--- /dev/null
+++ b/schemas/foambench_qoi_candidate.schema.json
@@ -0,0 +1,18 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "foambench_qoi_candidate.schema.json",
+  "title": "FoamBench QoI candidate observation",
+  "type": "object",
+  "required": ["schema_version", "case_id", "qois", "health"],
+  "properties": {
+    "schema_version": {"type": "string", "pattern": "^foambench\\.qoi\\.candidate(?:\\.v[0-9]+)?$"},
+    "case_id": {"type": "string", "minLength": 1},
+    "status": {"type": "string"},
+    "qois": {"type": "object", "additionalProperties": {"oneOf": [{"type": "number"}, {"type": "object"}]}},
+    "principal_metrics": {"type": "array", "items": {"type": "string"}},
+    "required_metrics": {"type": "array", "items": {"type": "string"}},
+    "missing_metrics": {"type": "array", "items": {"type": "string"}},
+    "health": {"type": "object", "required": ["status"], "properties": {"status": {"type": "string"}}, "additionalProperties": true}
+  },
+  "additionalProperties": true
+}
diff --git a/schemas/foambench_qoi_comparison.schema.json b/schemas/foambench_qoi_comparison.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..1923cf4b1e2d8c0e2c229da4289a473333078b7e
--- /dev/null
+++ b/schemas/foambench_qoi_comparison.schema.json
@@ -0,0 +1,22 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "foambench_qoi_comparison.schema.json",
+  "title": "FoamBench QoI comparison",
+  "type": "object",
+  "required": ["schema_version", "status", "physics_grounded_qoi_pass", "qoi_pass_ratio", "qoi_quality", "qoi_coverage_fraction", "metrics"],
+  "properties": {
+    "schema_version": {"const": "foambench.qoi.case_comparison.v3"},
+    "status": {"enum": ["pass", "incomplete", "out_of_tolerance", "incomplete_and_out_of_tolerance", "invalid_contract", "error"]},
+    "physics_grounded_qoi_pass": {"type": "boolean"},
+    "threshold_pass": {"type": "boolean"},
+    "qoi_pass_ratio": {"type": "number", "minimum": 0, "maximum": 1},
+    "qoi_quality": {"type": "number", "minimum": 0, "maximum": 1},
+    "qoi_coverage_fraction": {"type": "number", "minimum": 0, "maximum": 1},
+    "coverage_fraction": {"type": "number", "minimum": 0, "maximum": 1},
+    "metrics": {"type": "object"},
+    "group_scores": {"type": "object"},
+    "missing_metrics": {"type": "array", "items": {"type": "string"}},
+    "out_of_tolerance_metrics": {"type": "array", "items": {"type": "string"}}
+  },
+  "additionalProperties": true
+}
diff --git a/schemas/foambench_qoi_reference.schema.json b/schemas/foambench_qoi_reference.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..dc041b43b99c7eb5e2c3160789888f729316daa0
--- /dev/null
+++ b/schemas/foambench_qoi_reference.schema.json
@@ -0,0 +1,55 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "foambench_qoi_reference.schema.json",
+  "title": "FoamBench QoI reference contract",
+  "type": "object",
+  "required": ["schema_version", "cases"],
+  "properties": {
+    "schema_version": {"type": "string", "pattern": "^foambench\\.reference_qois(?:\\.v[0-9]+)?$"},
+    "cases": {
+      "type": "object",
+      "minProperties": 1,
+      "additionalProperties": {"$ref": "#/$defs/case"}
+    }
+  },
+  "additionalProperties": true,
+  "$defs": {
+    "case": {
+      "type": "object",
+      "required": ["principal_qoi_group", "principal_metrics", "qois", "tolerances"],
+      "properties": {
+        "principal_qoi_group": {"type": "string", "minLength": 1},
+        "principal_metrics": {"type": "array", "minItems": 1, "uniqueItems": true, "items": {"type": "string", "minLength": 1}},
+        "qois": {"type": "object", "minProperties": 1, "additionalProperties": {"oneOf": [{"type": "number"}, {"type": "object"}]}},
+        "tolerances": {"type": "object", "additionalProperties": {"$ref": "#/$defs/tolerance"}},
+        "metric_roles": {"type": "object", "additionalProperties": {"enum": ["principal", "scored", "diagnostic", "redundant"]}}
+      },
+      "additionalProperties": true
+    },
+    "tolerance": {
+      "type": "object",
+      "properties": {
+        "low": {"type": "number"},
+        "high": {"type": "number"},
+        "reference_value": {"type": "number"},
+        "relative_tolerance": {"type": "number", "minimum": 0},
+        "absolute_floor": {"type": "number", "minimum": 0},
+        "kind": {"type": "string"},
+        "relative_max": {"type": "number", "minimum": 0},
+        "normalized_rmse_max": {"type": "number", "minimum": 0},
+        "normalized_linf_max": {"type": "number", "minimum": 0},
+        "normalized_l1_max": {"type": "number", "minimum": 0},
+        "minimum_time_coverage": {"type": "number", "minimum": 0, "maximum": 1},
+        "normalization_floor": {"type": "number", "minimum": 0},
+        "maximum_cell_offset": {"type": "number", "minimum": 0},
+        "physical_floor": {"type": "number", "minimum": 0},
+        "provisional": {"type": "boolean"}
+      },
+      "anyOf": [
+        {"required": ["low", "high"]},
+        {"required": ["kind"]}
+      ],
+      "additionalProperties": true
+    }
+  }
+}
diff --git a/schemas/qoi_recovery_plan.schema.json b/schemas/qoi_recovery_plan.schema.json
new file mode 100644
index 0000000000000000000000000000000000000000..faf792819dde15931e28ac95b9bc49e9e953f4a5
--- /dev/null
+++ b/schemas/qoi_recovery_plan.schema.json
@@ -0,0 +1,28 @@
+{
+  "$schema": "https://json-schema.org/draft/2020-12/schema",
+  "$id": "qoi_recovery_plan.schema.json",
+  "title": "Conservative QoI recovery plan",
+  "type": "object",
+  "additionalProperties": false,
+  "required": ["status", "reason"],
+  "properties": {
+    "status": {"enum": ["recoverable", "unrecoverable", "uncertain"]},
+    "reason": {"type": "string"},
+    "mappings": {
+      "type": "array",
+      "items": {
+        "type": "object",
+        "additionalProperties": false,
+        "required": ["metric", "source", "operation"],
+        "properties": {
+          "metric": {"type": "string"},
+          "source": {"type": "string"},
+          "operation": {"enum": ["table_time_history", "branch_spalding_table"]},
+          "column": {"type": "string"},
+          "patch": {"type": "string"},
+          "branch_column": {"type": "string"}
+        }
+      }
+    }
+  }
+}
diff --git a/scripts/verify_release.py b/scripts/verify_release.py
new file mode 100644
index 0000000000000000000000000000000000000000..05d8bfe3b637ee12569fc52e8e4055cd36b24907
--- /dev/null
+++ b/scripts/verify_release.py
@@ -0,0 +1,48 @@
+"""Verify integrity, task projection, references and geometry; no solver runs."""
+import argparse
+import hashlib
+import json
+from pathlib import Path
+ROOT=Path(__file__).resolve().parents[1]
+def read(p):return json.loads(p.read_text(encoding='utf-8'))
+def require(ok,message):
+    if not ok:raise ValueError(message)
+def verify(root):
+    paths=set()
+    for line in (root/'SHA256SUMS').read_text(encoding='utf-8').splitlines():
+        digest,rel=line.split('  ',1);p=(root/rel).resolve()
+        require(p.is_relative_to(root.resolve()),f'Unsafe checksum path: {rel}')
+        require(p.is_file(),f'Missing file: {rel}')
+        require(hashlib.sha256(p.read_bytes()).hexdigest()==digest,f'Checksum mismatch: {rel}')
+        require(rel not in paths,f'Duplicate checksum path: {rel}');paths.add(rel)
+    source=read(root/'metadata/source_manifest.json')
+    for row in source['files']:
+        require(hashlib.sha256((root/row['path']).read_bytes()).hexdigest()==row['sha256'],f'Source drift: {row["path"]}')
+    coverage=read(root/'metadata/coverage.json');all_ids=set()
+    for track,expected in [('extended',100),('basic',110),('advanced',16)]:
+        profile=read(root/f'benchmarks/evaluation/profiles/{track}.json')
+        tasks=read(root/profile['benchmark_path']);refs=read(root/profile['reference_qois_path'])['cases'];stats=read(root/f'benchmarks/reference_statistics/{track}.json')['cases']
+        rows=[json.loads(line) for line in (root/f'data/{track}.jsonl').read_text(encoding='utf-8').splitlines()]
+        require(len(rows)==len(tasks)==expected,f'Count mismatch: {track}')
+        require(set(tasks)==set(refs)==set(stats)=={r['case_id'] for r in rows},f'Membership mismatch: {track}')
+        for row in rows:
+            cid=row['case_id'];require(row['task_id']==f'{track}:{cid}' and row['task_id'] not in all_ids,'Task ID collision');all_ids.add(row['task_id'])
+            require(row['usr_requirement']==tasks[cid]['usr_requirement'],f'Prompt drift: {cid}')
+            require(row['track']==track and row['family']==cid.split('/')[0],f'Metadata mismatch: {cid}')
+            origin='ExtFoamBench (EasyFoam authors)' if track=='extended' else 'FoamBench (upstream; adapted for OpenFOAM 13)'
+            require(row['task_origin']==origin,f'Attribution mismatch: {cid}')
+            require(row['external_asset_ids']==[a['asset_id'] for a in tasks[cid].get('_external_assets',[])],f'Asset ID drift: {cid}')
+            for metric in refs[cid].get('principal_metrics',[]):
+                require(metric in refs[cid].get('qois',{}) and metric in refs[cid].get('tolerances',{}),f'Missing metric contract: {cid}/{metric}')
+        require(sorted(k for k,v in stats.items() if not v)==coverage[track]['missing_numerical_statistics_case_ids'],f'Coverage drift: {track}')
+    specs=read(root/'benchmarks/FoamBench_extended_openfoam13_measurement_specs.json')
+    require(set(specs['cases'])==set(read(root/'benchmarks/FoamBench_extended_openfoam13_fixed.json')),'Measurement membership drift')
+    assets=read(root/'benchmarks/assets/manifest.json')['assets']
+    for asset_id,row in assets.items():
+        require(hashlib.sha256((root/row['path']).read_bytes()).hexdigest()==row['sha256'],f'Geometry mismatch: {asset_id}')
+    return {'status':'pass','tasks':len(all_ids),'copied_source_files':len(source['files']),'checksum_files':len(paths),'geometry_assets':len(assets)}
+def main():
+    parser=argparse.ArgumentParser(description=__doc__);parser.add_argument('--root',type=Path,default=ROOT);args=parser.parse_args()
+    try:print(json.dumps(verify(args.root.resolve()),indent=2))
+    except (OSError,ValueError,KeyError) as exc:parser.exit(1,f'Verification failed: {exc}\n')
+if __name__=='__main__':main()