|March 20, 2012, 06:16||
Pressure outlet (supersonic case)
Join Date: Oct 2010
Posts: 2Rep Power: 0
How to impose backflow pressure value for Pressure outlet in FLUENT for supersonic case?
As the variables are being extrapolated from inlet, I'm not able to forcefully impose the pressure value at the outlet.
I should study the effect of back pressures in a channel having supersonic flow inside it. (I'm using density based solver with Ideal gas law)
|cfd, pressure outlet, supersonic|
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