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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!
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