Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form /
By Jim A. Penland, Herbert W. Ridyard, and David E. Fetterman, Jr.

Description

Main Author

Penland, Jim A.

Related Names

Fetterman, David E.
Ridyard, Herbert W.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Lift (Aerodynamics)
Drag (Aerodynamics)
Airplanes > Airplanes / Wings, Trapezoidal.
Stability of airplanes, Longitudinal.
Hypersonic planes.

Note

"January 18, 1955."

Physical Description

27 p. : ill. ; 27 cm.

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