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Winglets Interview Question 737NG
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9th Feb 2010, 23:33
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QJB
Join Date: Aug 2009
Location: Australia
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Quote:
Induced Drag= Lift(squared) x Wing Span(squared) / Velocity of Aircraft(squared).
Don't you mean:
[0.318(CL^2/pi*AspectRatio*efficiencyfactor)]*q*s
J
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