Hi, I am solving a case
 

Hi,

I am solving a case with for an inlet of air breathing engine for mach 3 and for some combinations of Ramp and Claw i am getting undesired results.

Can Someone Tell me how are the equations differ betweene sonicTurbFoam and rhopSonicFoam.

i am a begnier in OpenFOAM so it may look a stupid question.

but as far as i know rhopSonicFoam does not take terbulance in to account.

Please suggest me anyone knows how to capture Shock reflections in OpenFOAM.