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Airfoil simulation

Question asked by reeshi pradhan on Feb 25, 2009
Latest reply on Feb 25, 2009 by Bill McEachern
I wanna use CosmosFlow to find out the drag and lift coeff. of NACA 0015.
When I ran the simulation, I got the weired result.
Do I need to create 3D model of Airfoil to analyse the above parameters.
and I wanna run simulation for angle of attack 0-15, how can I do this?

Cord = 1m
span length = 1m
angle of attack = 10