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how to get 2d cl and cd over a 3d wing?

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Old   September 27, 2013, 07:31
Default how to get 2d cl and cd over a 3d wing?
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Jaume Casas
Join Date: May 2013
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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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