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March 9, 2011, 08:11 |
2D wing in flotran
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Join Date: Mar 2011
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is there a way to find the lift created by a wing using flotran in ansys 12,1? ive set up a wind tunnel scenario in 2D and i would like to know how to calculate the Coefficient of lift and coefficient of drag but i dont know how to do it.
any replies would be much appreciated regards, stuart |
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flotran, lift coefficient, wing |
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