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Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /

Title:Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 /
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Note:Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]
  
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Subject:Mach number
Subject:Wings (Anatomy)
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