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Old 9th Feb 2010, 17:28
  #2881 (permalink)  
misd-agin
 
Join Date: Jan 2006
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The lift drag benefit can be examined by checking stall speeds. On every airliner I've checked(6 types), the first notch of flaps reduces stall speed by 50-60%.

Obviously the greater the deflection the more drag vs lift is created.

Any old school fighter pilot can tell you about the value of leading edge devices. "Hard wing" wasn't your friend in a turning(ie high AOA) fight.
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