0.2J 0.6 1 1.0 1 1> * -\A l-i.o _ -0.6 • -0.2 0.^ O.S 1.2 -1.2 -0.6 -OA 0 Fig.3. Vertical component of the disturbance velocity plotted against the lateral and the vertical distance from the wing. bi + b2 G/ coefficient of mutual. ir.flu.ence a = Dg/hi "~2 9v0
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