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Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces

Title:Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces
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Note:National Aeronautics and Space Administration, 1961
  
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Subject:Angle of attack (Aerodynamics)
Subject:Hypersonic planes, Military -- Models -- Testing
Subject:Stability of airplanes, Longitudinal -- Testing
Subject:Supersonic wind tunnels -- Testing
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