Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60° sweptback-wing--indented-body configuration at transonic speeds /
by Thomas L. Fischetti.

Description

Main Author

Fischetti, Thomas L.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1954.

Subjects

Stability of airplanes, Longitudinal.
Aerodynamics, Transonic.
Aerodynamics, Transonic.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Stability.
Stability of airplanes, Longitudinal.

Note

"June 17, 1954."

Physical Description

17 pages : illustrations ; 27 cm.

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