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NASA TN D-1793

Title:NASA TN D-1793
Alternate title:Center-line pressure distributions on two-dimensional bodies with leading-edge angles greater than that for shock detachment at Mach number 6 and angles of attack up to 25 ̊
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Note:National Aeronautics and Space Administration, 1963
  
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Subject:Angle of attack (Aerodynamics)
Subject:Shock waves
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