Turbulent simulation of Ramjet engine intake
I want to do RANS computation of Ramjet engine intake. The flow physics is some what complicated because there is a transition from supersonic to subsonic and also there will be oblique shock, shock reflection, shock-boundary layer interaction, and normal shock.
The RANS compressible solver available in OF 1.6 is all Pressure-based solver (correct me if i am wrong) and also transient.
My requirement is steady state, density based RANS solver
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