{"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": []}