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Forum: OpenFOAM

October 11, 2011, 09:00

Replies: 53

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

Views: 14,454

Posted By praveen

Maybe it needs more iterations to reach steady...

Maybe it needs more iterations to reach steady state. Note that rhoCentralFoam uses global time stepping, so reaching steady state can be very slow. And moreover it uses forward euler time stepping....

Forum: OpenFOAM

October 7, 2011, 23:59

Replies: 53

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

Views: 14,454

Posted By praveen

Use rhoCentralFoam. That is good for shock...

Use rhoCentralFoam. That is good for shock capturing and compressible flows.

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