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Calculating additional lift from deploying flaps

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rtfm

Well-Known Member
Joined
Jan 3, 2008
Messages
3,900
Location
Brisbane, Australia
Hi,
I'm sure Raymer covers this in his books (I have both - however I can't follow the math in his big book, and my home-builders version is out on loan). So can anyone help me out? I'm trying to calculate the amount of additional lift per degree if possible, provided by the deployment of flaps. Or of ailerons.

Thanks,
Duncan
 
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