Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels / by M. Leroy Spearman and Gerald V. Foster.
|Main Author:||Spearman, M. Leroy.|
|Other Authors:||Foster, Gerald V.|
Washington, D.C. : National Aeronautics and Space Administration, 1961.
> Wings, Swept-back.
Airplanes > Wings, Triangular.
Stability of airplanes, Longitudinal.
Stability of airplanes, Lateral.
Vertically rising aircraft > Aerodynamics.
Short take-off and landing aircraft.
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31 p. :
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