Investigation of the lift, center of pressure, and drag of a projectile at Mach number of 8.6 and a Reynolds number of 17 million /
by Thomas N. Canning.

Description

Main Author

Canning, Thomas N.

Related Names

Ames Research Center.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

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

Subjects

Drag (Aerodynamics)
Lift (Aerodynamics)
Reynolds number.
Aerodynamics, Hypersonic.

Note

"November 19, 1954."

Physical Description

18 p. : ill. ; 27 cm.

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