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Inviscid flow in a Laval nozzle

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Old   August 3, 2007, 04:24
Default Inviscid flow in a Laval nozzle
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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?

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Old   August 3, 2007, 05:46
Default Re: Inviscid flow in a Laval nozzle
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Grid sensitivity checks.

Convergence sensitivity checks.

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