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Forum: OpenFOAM

November 2, 2011, 12:30

Replies: 53

No shock in airfoil 0012 case despite of Mach number exceeds 1

Views: 14,414

Posted By Technoyoungman

Hi Nils Droeske On Youtube...

Hi Nils Droeske

On Youtube (http://www.youtube.com/watch?v=49sOQ89v-O8) you can see my simulation of intake system of aircraft with 500m/c velocity, 100kPa pressure and 300K temperature....

Forum: OpenFOAM

November 2, 2011, 05:53

Replies: 53

No shock in airfoil 0012 case despite of Mach number exceeds 1

Views: 14,414

Posted By Technoyoungman

Have you checked the stagnation parameters?

Dear Schwermetall,
After the simultion, did you happen to check the total pressure and total temperature? I think u should check. I would like to know the result. When I run supersonic flow,...

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