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Lift Coefficient

Question asked by reeshi pradhan on Feb 26, 2009
Latest reply on Feb 27, 2009 by reeshi pradhan
Which equation is to be used to find Lift Coeff. of airfoil in Floworks?
This is equation I had used.
But result vary.

{GG Y - Component of Force 1}/(Re*Dynamic viscosity)^2* span length of airfoil)*(2*density of air*Cord length)

Velocity in term of reynold's no.