Effect of aileron displacement on wing characteristics

Heald, R H (Bureau of Standards)
naca-tn-448
February 1933


The effect of aileron displacement on wing characteristics has been investigated for the Clark Y and the U.S.A. 27 wing sections equipped with rectangular ailerons. The airfoils, rectangular in plan, and having a 10 inch chord and 60 inch span, were mounted on a model fuselage.

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