Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept back 63 deg - Characteristics Throughout the Subsonic Speed Range with the Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25

J. Lloyd Jones, Fred A. Demele
naca-rm-a9d25
Aug 1949


Wind-tunnel tests have been made to determine the independent effects of Mach and Reynolds numbers on the aerodynamic characteristics of a wing-fuselage combination employing a wing having the the leading edge swept back 63 deg and having camber and twist. Tests were also made of the fuselage alone.

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