Catalog Record: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design | Hathi Trust Digital Library

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Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design / by Odell A. Morris and Gerald V. Foster.

Main Author: Morris, Odell A.
Other Authors: Foster, Gerald V.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1961.
Subjects: Hypersonic planes, Military > Testing.
Airplanes > Wings, Swept-back > Testing.
Stability of airplanes, Longitudinal > Testing.
Stability of airplanes, Lateral > Testing.
Angle of attack (Aerodynamics)
Supersonic wind tunnels > Testing.
Note: Cover title.
"April 1961."
Full text also available online. Address as of 11/16/2010:
Physical Description: 28 p. : ill. ; 26 cm.
Original Format: Book
Locate a Print Version: Find in a library
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