Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel /
By Eugene S. Love, Donald E. Coletti, and August F. Bromm, Jr.

Description

Main Author

Love, Eugene S.

Related Names

Bromm, August F.
Coletti, Donald E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1952.

Subjects

Aerodynamics, Supersonic.
Body of revolution.
Base flow (Aerodynamics)
Drag (Aerodynamics)
Reynolds number.

Note

"October 17, 1952."

Physical Description

62 p. : ill. ; 27 cm.

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