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.

Description

Main Author

Bingham, Gene J.

Related Names

Braslow, Albert L.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1954.

Subjects

Airplanes > Airplanes / Fuselage.
fuselages.
Airplanes > Airplanes / Fuselage.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Handling characteristics.

Note

On front cover: "Classification Changed to Unclassified, Authority: NACA Research Abstract No. 97. Effective Date; February 25, 1955 WHL."
On front cover: "April 5, 1954."

Physical Description

10 pages : illustrations ; 27 cm.

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