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Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : characteristics throughout the subsonic speed range with the wing cambered and twisted for a uniform load at a lift coefficient of 0.25

Jenny L. Jones, Fred A Demele

Abstract

Report presenting wind-tunnel testing to determine the independent effects of Mach and Reynolds numbers on the aerodynamic characteristics of a wing-fuselage combination with a wing with the leading edge swept back 63 degrees and with camber and twist. Results regarding the fuselage alone and the effects of camber and twist are also provided.

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Available abstract

Key concepts: Fuselage, Wing, Wing twist, Camber (aerodynamics), Aerodynamics, Airfoil, Structural engineering, Mach number