hypersonic inlet
 

Hi all,
I am doing a simulation of hypersonic inline compression inlet at mach no.= 7 at an altitude of 35 km.

I have taken solver as density based, implicit,2D , steady, absolute.
Density as ideal gas and tried with operating pressure of 0 atm, pressure inlet & pressure outlet.

The results are not converging... Pls help...

Regards,
vivek