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Old   October 11, 2010, 07:45
Question Pls help
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Sreedevi Radhakrishnan
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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 in solve- monitors-force.
The problem is with Report- Reference values. There what values should be given for area and length? Please help me
Thanks in advance
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3d airfoil, reference values

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