Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers /
John C. Wilson and Henry L. Kelley.

Description

Main Author

Wilson, John C.

Related Names

Kelley, Henry L.
United States. Army Aviation Research and Technology Activity.
Langley Research Center.
United States. Army Aviation Systems Command.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

[Washington, DC] : National Aeronautics and Space Administration, 1986.

Subjects

Spoilers.
Tail helicopter rotors.
Tails (Aircraft)
Aeronautical booms.
Wind tunnel tests.
Aerodynamics.
Helicopters > Helicopters / Tails.

Note

STAR Subject category 02.
"January 1986."

Physical Description

72 p. : ill. ; 28 cm.

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