The effect of body contouring on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail and several wing-fuselage combinations having sweptback wings of relatively high aspect ratio

Sutton, Fred B., Lautenberger, J. Walter, Jr.
naca-rm-a56j08
1957


An investigation was conducted in the Ames 12 foot pressure wind tunnel to determine the effect of a realtively simple Kuchemann type fuselage modification at the wing-fuselage juncture of several sweptback wing-fuselage and wing-fuselage-tail combinations.

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