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Forum: FLUENT

July 15, 2011, 09:43

Replies: 5

compressible flow in a duct - supersonic inlet mach number

Views: 3,070

Posted By charndrabose_mit

no am not an expert n combustion ..

no am not an expert n combustion ..

Forum: FLUENT

July 7, 2011, 04:20

Replies: 5

compressible flow in a duct - supersonic inlet mach number

Views: 3,070

Posted By charndrabose_mit

BC's Needed for Supersonic flow through a duct

thanks a lot Mr. Adrien...

I have tried the way as given in the fluent tutorial. But still not able to capture the shock wave reflections.. Can you please let me know the settings for the inlet...

Forum: FLUENT

July 2, 2011, 05:05

Replies: 5

compressible flow in a duct - supersonic inlet mach number

Views: 3,070

Posted By charndrabose_mit

compressible flow in a duct - supersonic inlet mach number

Dear All.... I have tried out the simulation of compressible flow (Mach=3) through a constant area duct (both 2D and 3D) in fluent . But i could not able to predict the variations properly (shock...

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