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 and Albert L. Braslow.

APA Citation

Bingham, G. J., Braslow, A. L., Langley Aeronautical Laboratory., United States. National Advisory Committee for Aeronautics. (1954). 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. Washington, D.C.: National Advisory Committee for Aeronautics.

MLA Citation

Bingham, Gene J, Albert L Braslow, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics. 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. Washington, D.C.: National Advisory Committee for Aeronautics, 1954.

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