Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds

Fred B. Sutton, Andrew Martin
naca-rm-a50j26a
Feb 1951


As part of an NACA transonic research program, a series of wing-fuselage combinations varying chiefly in wing plan form is being investigated. In the part of the investigation reported herein, three representative model wings of the series were tested at Mach numbers up to 0.94 in the Ames 16-foot high-speed wind tunnel.

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