What solver to use for inviscid flow simulation over missile
i want to solve steady inviscid flow simulation over missile
transonic & supersonic case
rhopSonicFoam & rhoSonicFoam, these two for inviscid flow, but they are transient solver. Is there a way to convert these solver to steady state or is it possible to use large time step.
Also, the slip boundary condition behaviour in OpenFoam. is it the right boundary condition for inviscid flow?
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