|November 12, 2014, 20:56||
SimpleFOAM: 3D NACA0012 WING
Join Date: Apr 2014
Posts: 7Rep Power: 3
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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