A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements /
by Eugene D. Schult.

Description

Main Author

Schult, Eugene D.

Related Names

Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

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

Subjects

Drag (Aerodynamics)
Rolling (Aerodynamics)
Airplanes > Airplanes / Control systems.
Spoilers (Airplanes)

Note

"September 20, 1955; Declassified May 29, 1959."

Physical Description

35 p. : ill. ; 27 cm.

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