Wind tunnel test for elevator hinge moment coefficients on the horizontal tail surface no. 5 with balanced elevator (supplementary to Serial Report 2463, A.S. Information Circular, Vol. 6, No. 511) (airplane section report)
Lyons, P. M.
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DescriptionThis document is a supplement to Air Service Information Circular, Vol. 6, No. 511, Wind tunnel test of six horizontal tail surface designs having the U.S.A.-47 airfoil section (airplane section report). The object of this test was to determine the elevator moments about the hinge line on this balanced tail surface.
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