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Center of Pressure on a Slotted Flap

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A

aircraft

Well-Known Member
Joined
Jul 17, 2013
Messages
55
Location
Fremont, CA/USA
For a one-section airfoil, Center of Pressure (C.P.) is around quarter chord. We can assume its range is 0.23-0.27 for structural design. Where is the C.P. for a slotted flap? Does the main section ahead change the location? Pointers to papers on this would also be highly appreciated.
 
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