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I have my ailerons reflexed about 3 deg up. As I have
posted in the past, through testing I found that varying the flap reflex with
weight and density altitude could result in a 1.5% change of speed. The higher
the density altitude and the higher the weight, the less reflex should be
employed in order to increase the wing's camber for the higher required CL. As
camber is changed on the NLF1 015F airfoil, the drag bucket moves along with it.
You will also have an added benefit of the fuselage angle being reduced which
gives better visibility over the nose.
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