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Thread: Winglets Interview Question 737NG
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Old 9th February 2010 | 23:33
  #5 (permalink)  
QJB
 
Joined: Aug 2009
Posts: 92
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From: Australia
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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