Hi, I am solving a case
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.
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