Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /
by Gerald V. Foster.

Description

Main Author

Foster, Gerald V.

Related Names

United States. National Aeronautics and Space Administration.

Language(s)

English

Published

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

Subjects

Aerodynamics, Supersonic.
Spoilers (Airplanes) > Spoilers (Airplanes) / Performance.
Airplanes > Airplanes / Wings, Swept-back.
Stability of airplanes.

Note

"April 1960."
Cover title.

Physical Description

15 p. : 5 ill. ; 27 cm.

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