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Air Force and Three Moments for F-5-L Seaplane (1922)

NASA Technical Reports Server (NTRS) · leaf 15

An illustration from Air Force and Three Moments for F-5-L Seaplane, 1922, leaf 15
*9 a.) Deflection of aileron from wing chord. Fig. 6. Rolling moment at various positions of ailerons. Axis of hull parallel to wind. Wind speed 4-0 in.p.h.

NASA Technical Reports Server (NTRS)

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