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1.59 and angles of attack up to 36°

Title:1.59 and angles of attack up to 36°
Alternate title:A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36°
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Note:National Advisory Committee for Aeronautics, 1952
  
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Subject:Aerodynamic load
Subject:Angle of attack (Aerodynamics)
Subject:Body of revolution
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