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The aerodynamic wind vane and the inherent stability of airplanes (1931)

NASA Technical Reports Server (NTRS) · leaf 17

An illustration from The aerodynamic wind vane and the inherent stability of airplanes, 1931, leaf 17
N.A.C.A. Technical Memorandiam No.607 Pigs.1.4,6,8 … Fig.4 Mounting of horizontal tail surfaces for measuring hinge moments. Fig. 8 Mounting of model for measuring rolling moments. for-is Office. f^.A.e.A. Fig.5 Mounting of model for measuring yawing moments.

NASA Technical Reports Server (NTRS)

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