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Forum: FLUENT October 11, 2010, 07:45

Replies: 0 Pls help Views: 1,543 Posted By bluey Pls help I want to calculate lift and drag coefficients for a 3D airfoil. My airfoil has got thickness so hope i can consider it as 3D. The angle of attack is 15 degrees so i have resolved the force vectors...

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