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Thread: Glide AoA vs. Drag
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Old 20th October 2011 | 08:10
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Captain Sand Dune
 
Joined: Jun 2001
Posts: 984
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From: Victoria
appendages to the fuselage
wuold increase zero loft drag only. The effect on the total lift curve would be to move the EAS for best L/D left. Therefore I reckon the EAS for best L/D would decrease, with a corresponding increase in AoA.
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