Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IV : floating tip ailerons on rectangular wings (1933)
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484 EEPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS in coefficient form in Tables V, VI, Vii, and VJUUL. effect of the flaps on maximum lift was small, the flap The triangular end plates increased the maximum settings were in most of the cases varied throughout a lift slightly and decreased the… … Flap angle, irailing edge up Figube 2.—Variation of maxlrnnm lift and the ratio of max- imum lift to minimum drag with flap angle. Clark Y airfoil with N. A. C. A. 0010 symmetrical tip floating ailerons also improved the control at 20° yaw. The circular end plates increased the maximum lift, but…
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