Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶, by Gene J. Bingham et al.

Title:	Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45° sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶
Author:	Bingham, Gene J.
Author:	Braslow, Albert L.
Author:	Langley Aeronautical Laboratory
Author:	United States. National Advisory Committee for Aeronautics
Note:	Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954

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Subject:	Airplanes -- Fuselage
Subject:	Airplanes -- Wings, Swept-back -- Handling characteristics
Subject:	Fuselages
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