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...
|All times are GMT -4. The time now is 00:32.|