I am a new user to OF. I am interested in using OF as an viscous or inviscid solver for hi enthalpy hypersonic flows where the chemistry behind the bow shock is considered. That is, not only high Mach number but the ability to simulate chemical non-equilibrium. Is there a solver available for this purpose? If not, how difficult would it be to develop such a thing?
I am also in need of Steady state compressible flow solver for transonic and supersonic flows.
rhoSimpleFoam handled subsonic case well, Is it possible to use rhoSimpleFoam for transonic & supersonic case. If so what the solver settings.
I searched in the forum, but not able to get solution for my problem. Some one reply Plz.
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