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 et al.

Title:	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
Author:	Morris, Odell A.
Author:	Foster, Gerald V.
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1961

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Subject:	Airplanes -- Wings, Swept-back -- Testing
Subject:	Angle of attack (Aerodynamics)
Subject:	Hypersonic planes, Military -- Testing
Subject:	Stability of airplanes, Lateral -- Testing
Subject:	Stability of airplanes, Longitudinal -- Testing
Subject:	Supersonic wind tunnels -- Testing
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