|February 25, 2011, 06:17||
Join Date: Feb 2011
Posts: 2Rep Power: 0
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...
|hypersonic, inlet and outlet pressure, inlet gauge pressure, outlet, outlet boundary|
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