The tutorial demonstrates generation of a C-grid mesh using blockMesh The geometry is provided by a surface mesh (OBJ file) of the NACA0012 aerofoil The case is setup with a freestream flow speed of Ma=0.72 Thanks to Kai Bastos at Duke University for the geometry and helpful input. |
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overRhoSimpleFoam/hotCylinder | ||
rhoCentralDyMFoam/movingCone | ||
rhoCentralFoam | ||
rhoPimpleAdiabaticFoam/rutlandVortex2D | ||
rhoPimpleFoam | ||
rhoPorousSimpleFoam/angledDuct | ||
rhoSimpleFoam | ||
sonicDyMFoam/movingCone | ||
sonicFoam | ||
sonicLiquidFoam |