Damping in roll of models with 45°, 60°, and 70° delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models /
By. E. Claude Sanders, Jr.

Description

Main Author

Sanders, E. Claude.

Related Names

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

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1952.

Subjects

Vibration (Aeronautics) > Vibration (Aeronautics) / Damping.
Stability of airplanes, Lateral.
Rolling (Aerodynamics)
Airplanes > Airplanes / Wings, Triangular.
Stability of airplanes, Lateral.
Rolling (Aerodynamics)
Vibration (Aeronautics) > Vibration (Aeronautics) / Damping.
Airplanes > Airplanes / Wings, Triangular.

Note

"June 25, 1952; Declassified April 6, 1956."

Physical Description

18 pages : illustrations ; 27 cm

Locate a Print Version

Find in a library

Viewability