Aerodynamic-derivative characteristics of the X-15 research airplane as determined from flight tests for mach numbers from 0.6 to 3.4 /
by Roxanah B. Yancey, Herman A. Rediess and Glenn H. Robinson.

Description

Main Author

Yancey, Roxanah B.

Related Names

United States. National Aeronautics and Space Administration.

Language(s)

English

Published

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

Subjects

Stability and control.
Simulators and computers.
Piloting.
Aircraft.
Aerodynamics, missiles and space vehicles.
Aerodynamics, aircraft.

Note

Cover title.
"January 1962."
Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Aircraft; Piloting;Simulators and computers; Stability and control.

Physical Description

68 p.: ill. ; 26 cm.

Locate a Print Version

Find in a library

Viewability