analyzing NACA 0012 airfoil -- CFD Online Discussion Forums

March 24, 2007, 09:18	analyzing NACA 0012 airfoil	#1
Hammam Guest Posts: n/a	Hi everybody! i would like to analyze the NACA 0012 airfoil to determine the lift and drag coefficients at different angle of attack by using cfx. can you please tell me the steps required to achieve that. thanks M.Hammam.

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