Spinning characteristics of wings 1: rectangular Clark Y monoplane wing
Description:
"A series of wind tunnel tests of a rectangular Clark Y wing was made with the NACA spinning balance as part of a general program of research on airplane spinning. All six components of the aerodynamic force and moment were measured throughout the range of angles of attack, angles of sideslip, and values omega b/2v likely to be attained by a spinning airplane; the results were reduced to coefficient form. It is concluded that a conventional monoplane with a rectangular Clark y wing can be made …
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Date:
November 21, 1934
Creator:
Bamber, M. J. & Zimmerman, C. H.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department