Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds /
by James W. Wiggins and Richard E. Kuhn.

Description

Main Author

Wiggins, James W.

Related Names

Kuhn, Richard E.
United States. National Adviosry Committee for Aeronautics.
Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

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

Subjects

Airplanes > Airplanes / Wings, Swept-back.
Aerodynamics.
Aerodynamic load.
aerodynamics.
Aerodynamics.
Airplanes > Airplanes / Wings, Swept-back.
Aerodynamic load.

Note

"November 6, 1953."
Cover title.

Physical Description

xx pages : illustrations ; 27 cm.
22 pages : illustrations ; 27 cm.

Locate a Print Version

Find in a library

Viewability