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October 11, 2010, 08:45	Pls help	#1
bluey New Member Sreedevi Radhakrishnan Join Date: Oct 2010 Posts: 1 Rep Power: 0	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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