Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0 /
John C. McFall, Jr.

Description

Main Author

McFall, John C.

Related Names

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

Language(s)

English

Published

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

Subjects

Stability of airplanes, Longitudinal.
Aerodynamic load.
Airplanes > Airplanes / Wings, Swept-back.
Airplanes > Airplanes / Models > Airplanes / Models / Testing.

Note

"January 4, 1954."

Physical Description

34 p. : ill. ; 27 cm.

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