how to get 2d cl and cd over a 3d wing? -- CFD Online Discussion Forums

September 27, 2013, 07:31	how to get 2d cl and cd over a 3d wing?	#1
acasas Member Antonio Casas Join Date: May 2013 Location: world Posts: 85 Rep Power: 12	Hi. Fluent, after calculation, provide me the WHOLE CL and CD, in my case, over a 3d wing shape. Can anyone tell me how to print out the value for cl and cd per unit lenght of the cross section at diferent locations of the wing span? Thank´s

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