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High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds

Title:High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds
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Note:National Aeronautics and Space Administration ;, 1975
  
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Subject:Aerodynamics, Transonic
Subject:Aerofoils -- Testing -- Statistics
Subject:Reynolds number
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