Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° /
by M. Leroy Spearman and Gerald V. Foster.

Description

Main Author

Spearman, M. Leroy.

Related Names

Foster, Gerald V.
Langley Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, [D.C.] : National Aeronautics and Space Administration, 1959.

Subjects

Stability of airplanes.
Mach number.
Airplanes > Airplanes / Wings, Swept-back.

Note

"August 1959."
Cover title.

Physical Description

18 p. : ill. ; 26 cm.

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