Inviscid flow in a Laval nozzle
Hi, I'm trying to simulate an inviscid subsonic flow in a Laval nozzle, I aspect to have a 100% pressure recovery at the end of the divergent since the inlet area is equal to the outlet one. Still I am getting a pressure loss (actually about 2% of the pressure drop in the throat). I am using a segregated pressure based solver. Does anybody know how to fix it?
tnx |
Re: Inviscid flow in a Laval nozzle
Grid sensitivity checks.
Convergence sensitivity checks. etc. |
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