{"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": []}