Turbulent simulation of Ramjet engine intake
 

Hi all,

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

Regards
mecbe