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Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /

Title:Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method /
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Note:Washington, [D.C.] : National Aeronautics and Space Administration, 1960
  
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Subject:Steels
Subject:Magnesium
Subject:Mach number
Subject:Aluminum
Subject:Aircraft stability
Subject:Wing profiles
Subject:Vibration damping
Subject:Supersonic flutter
Subject:Supersonic airfoils
Subject:Free vibration
Subject:Control surfaces
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