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Forum: OpenFOAM Running, Solving & CFD

September 26, 2019, 12:52

Replies: 11

NACA 0012 Airfoil, simpleFoam, Spalart Allmaras

Views: 4,931

Posted By Artur.Ant

Remember also that if you are interested in drag...

Remember also that if you are interested in drag it is very important to solve correctly the velocity near the wall.
You should solve viscous sublayer with k-omega or k-omegaSST (how sheaker has...

Forum: OpenFOAM Running, Solving & CFD

September 26, 2019, 12:48

Replies: 11

NACA 0012 Airfoil, simpleFoam, Spalart Allmaras

Views: 4,931

Posted By Artur.Ant

You can also try to pass to more accurate...

You can also try to pass to more accurate divSchemes.
Have you tried to use Gauss linear for all div(...)?

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