Wind-tunnel investigation at Mach numbers from 1.60 to 2.86 of the static aerodynamic characteristics of a supersonic transport configuration with variable-sweep wings employing a double inboard pivot /
David S. Shaw and William P. Henderson.

Description

Main Author

Shaw, David S.

Related Names

Henderson, William P.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, [1962?]

Subjects

Supersonic wind tunnels > Supersonic wind tunnels / Testing.
Stability of airplanes, Longitudinal > Stability of airplanes, Longitudinal / Testing.
Airplanes > Airplanes / Wings, Swept-back > Airplanes / Wings, Swept-back / Stability > Airplanes / Wings, Swept-back / Stability / Testing.

Note

Cover title.
Full text also available online. Address as of 11/18/2010:

Physical Description

40 p. : ill. ; 26 cm.

Locate a Print Version

Find in a library

Viewability