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March 28, 2012, 20:32	NACA 0012 lift and drag coefficient.	#1
Tom Lucius New Member Tan Join Date: Dec 2011 Posts: 10 Rep Power: 14	I am running ANSYS fluent simulation flow over naca 0012 airfoil. So far the lift coefficient is similar with the published papers. The problem is drag coefficient is different so much in term of value compared to published papers. I have check my mesh quality and boundary condition, it shows no problem. Any idea why drag coefficient is different ???

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