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#1
January 1st 05, 11:32 PM
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Greg Esres wrote:
How did you arrive at 1.5%? L = Wcos(theta) *If* you assume level and climb airspeeds are the same. [zap: induced drag disagreement] (If you would read something other than Aerodynamics for Naval Aviators, you'd understand this.) Yeah, I also hate it when people use decades of research, hours of wind tunnel testing, and accepted aerodynamic principals in these newsgroups.  Hilton 
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