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Improvement of aileron effectiveness by the prevention of air leakage through the hinge gap as determined in flight (1938)

NASA Technical Reports Server (NTRS) · leaf 12

An illustration from Improvement of aileron effectiveness by the prevention of air leakage through the hinge gap as determined in flight, 1938, leaf 12 — Air speed, ft. per sec. figure 6.- Maximum rolling velocities obtained with 0.18c and 0.09o aileronsr

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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