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In a message dated 11/2/2007 5:56:36 P.M. Central Daylight Time,
elippse@sbcglobal.net writes:
From my experiments, the in-flight flap
reflex position is a function of required CL which in turn is related to weight, TAS, and density
altitude. I can change my flap reflex position by 2 deg. which will
change TAS by 3mph; I've done this over and over. This is due to the
relationship between parasite CD and camber
of the NLF1 0215F airfoil. Use maximum reflex when fast,
light, and low, and reduce it when slower, heavy, and
high!
You Bet, Paul.
There are not too many airplanes that give one such
interesting control over the performance by changes the shape of the wing
thru flap positions (uh, this includes trimming for ugly CG problems).
Other flapper-doodles are only designed to assist in the Cl at approach/landing
speeds.
We are lucky to be flying one of the more interesting wings extant.
Grayhawk
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