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.|
Washington, D.C. : National Aeronautics and Space Administration, 1961.
Hypersonic planes, Military
Airplanes > Wings, Swept-back > Testing.
Stability of airplanes, Longitudinal > Testing.
Stability of airplanes, Lateral > Testing.
Angle of attack (Aerodynamics)
Supersonic wind tunnels > Testing.
Full text also available online. Address as of 11/16/2010:
28 p. :
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