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Fin loads and tip-control hinge moments on a 1/8-scale model simulating the first stage of the Scout research vehicle at a mach number of 2.01

Title:Fin loads and tip-control hinge moments on a 1/8-scale model simulating the first stage of the Scout research vehicle at a mach number of 2.01
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Note:National Aeronautics and Space Administration, 1960
  
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Subject:Aerodynamics, Supersonic
Subject:Hinge moments (Aerodynamics)
Subject:Rockets (Aeronautics) -- Fins
Subject:Scout launch vehicles -- Stages -- Aerodynamics
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