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.

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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