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SimpleFOAM: 3D NACA0012 WING

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Old   November 12, 2014, 20:56
Default SimpleFOAM: 3D NACA0012 WING
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Dear Foamers

I am trying to simulate flow past a NACA0012 wing. Can anyone suggest a solved case of the similar type ? I am having trouble with the boundary conditions and it seems like the Cm, Cl and Cd are off charts. The Cl is too low and the Cd is relatively higher.

Thanks in advance.
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