Stability and control characteristics at a Mach number of 1.97 of an airplane configuration having two types of variable- sweep wings /
by Gerald V. Foster and Odell A. Morris.

Description

Main Author

Foster, Gerald V.

Related Names

Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, [D.C.] : National Aeronautics and Space Administration, 1960.

Subjects

Mach number.
Stability of airplanes.
Supersonic wind tunnels.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Testing.

Note

"August 1960."
Cover title.

Physical Description

43 p. : ill. ; 26 cm.

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