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Development of the NACA slot-lip aileron (1935)

NASA Technical Reports Server (NTRS) · leaf 22

An illustration from Development of the NACA slot-lip aileron, 1935, leaf 22
N.A.C.A. Fig. 9 … '-60 -50 -40 -30 -30 -10 0 10 30 30 Aileron deflection, 6A> degrees Figure 9.- Hinge-moment coefficients of a slot-lip aileron at 0.30 ohord with a speoial-shaps slot of slot gap 0.042o and slot width O.O660 with various aileron hinge-axis positions.

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