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Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60

Title:Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60
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Note:National Advisory Committee for Aeronautics, 1949
  
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Subject:Aerofoils
Subject:Lift (Aerodynamics)
Subject:Pitching (Aerodynamics)
Subject:Wind tunnel testing
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