$FOAM_TUTORIALS/discreteMethods/dsmcFoam/wedge15Ma5
We calculate the mixture gas flow of oxygen and nitrogen with the Direct Simulation Monte Carlo (DSMC) method. The Direct Simulation Monte Carlo (DSMC) method was proposed by G. A. Bird in the 1960s to calculate the flow of rarefied gases using the Boltzmann equation.
The properties of the gas are defined in the file "dsmcProperties" in the directory "constant", and the initial state is defined in the file "dsmcInitialiseDict" in the directory "system".
The model geometry is as follows: width 45.7 cm, height 30.0 cm, depth 0.84 cm. Among the boundaries, the region "flow" is assumed to be a flow velocity of (1736, 0, 0) m/s and the region "obstacle" is assumed to be a no-slip wall.
We have configured the file "controlDict" in the directory "system" to use a function object to output the forces and moments acting on the region "obstacle" at each time. These values are output as a file "forces.dat" in the directory "postProcessing/forces1/0".
Each variable in directory 0 is as follows.
Meshes are created before the calculation. The meshes are as follows.
The calculation result is as follows.
As explained earlier, the forces and moments acting on the region "obstacle" at each time are output to the file postProcessing/forces1/0/forces.dat. The forces and moments are output as pressure, viscous, and porous contribution (porous).
When combining the divided data in each processors using the command reconstructPar, we added the option "-noLagrangian" to prevent unnecessary Lagrangian data from being combined.
2 minutes 51.54 seconds *4 parallel, Inter(R) Core(TM) i7-2600 CPU @ 3.40GHz 3.40GHz