Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75° /
by Gerald V. Foster.

Description

Main Author

Foster, Gerald V.

Related Names

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.
Airplanes > Airplanes / Wings, Swept-back.
Aerodynamics, Supersonic.
Stability of airplanes > Stability of airplanes / Testing.

Note

"January 1960."
Cover title.

Physical Description

34 p. : ill. ; 26 cm.

Locate a Print Version

Find in a library

Viewability