Has anyone EVER managed to run: compressible steady state subsonic internal flow
If so, I would like to know which solver you used, and , if possible, see your input files...thanks!
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Hi,
I´ve tried this with the solver "rhoCentralFoam". At the inlet I took fixed Value for Temperature and velocity, at the outlet for pressure. I think my Mach number was 0.6. Steady state worked for simple geometries. For which cases are you doing this? regards treima |
I'm trying to use rhoSimplecFoam for a duct with an inlet and an outlet.
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