Learning Forum

[deb_biswas]

Hi, good people.

I am simulating biconvex 2D airfoil for supersonic flow. For high speed flow thickness of boundary layer is very low, viscous effect can be negligible. So we can apply inviscid theorem to solve governing equation. Now in sst k omega turbulence model, how I select inviscid fluid?

Thanks.

[aitor.amatriain]

You can modify that in Setup - Models - Viscous - Inviscid (first option)