Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75 degree and 108 degree, by Ross B. Robinson et al.

Title:	Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75 degree and 108 degree
Alternate title:	Stability and control characteristics at a Mach number of 1.41 of a variable-sweep airplane configuration capable of low-level supersonic attack-outer wing swept 75°and 108°
Author:	Robinson, Ross B.
Author:	Howard, Paul W.
Author:	Langley Research Center
Note:	National Aeronautics and Space Administration, 1960

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Subject:	Aerodynamics -- Testing
Subject:	Jet fighter planes -- Wind tunnel testing
Subject:	Mach number -- Testing
Subject:	Statics -- Testing
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