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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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Antonio Casas
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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?
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