Obtaining Coefficient of Lift and Drag -- CFD Online Discussion Forums

February 12, 2010, 12:14	Obtaining Coefficient of Lift and Drag	#1
Atella New Member Join Date: Jan 2010 Posts: 8 Rep Power: 16	Hi, I am investigating the performance of an aircraft wing and I need to find out the Coefficients of Lift and Drag for the wing. I am able to run a simulation and obtain the contour and vector plots but I am unable to find if there is a part to CFX which will give me a value for the Cl of Cd. If anyone would know how i could get this out it would be much appreciated. Thanks

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