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#1
September 19th 05, 07:38 PM
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Rotor lift coefficient
I have been trying to model rotor wake using vortex methods, I am
confused regarding the lift coefficient, should the value of the lift coefficient obtained after computing the lift using the bound vortex strength of the blade be the same as the sectional lift coefficient of the airfoil? 
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#2
September 25th 05, 01:17 AM
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