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!

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.