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Forum: OpenFOAM

June 8, 2011, 06:01

Replies: 17

NACA0012 with rhoCentralFoam

Views: 6,096

Posted By naveen

NACA0012 with rhoCentralFoam

hi praveen,

I got the proper results for airfoil using rhoCentralFoam for unstructured grid same as structured grid.

Regards

NAVEEN

Forum: OpenFOAM

June 3, 2011, 05:27

Replies: 17

NACA0012 with rhoCentralFoam

Views: 6,096

Posted By naveen

NACA0012 with rhoCentralFoam

OK....letś try some other way....can u give me your mail id....

NAVEEN.K.M

Forum: OpenFOAM

June 3, 2011, 05:07

Replies: 17

NACA0012 with rhoCentralFoam

Views: 6,096

Posted By naveen

NACA0012 with rhoCentralFoam

hi praveen,

I am also trying for different airfoil simulation using rhoCentralFoam using different boundary condition at mach no=0.7. even i am also getting same error wat u r getting on airfoil...

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