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Effects of flanges on pressure distribution on a flat plate and on a corrugated surface at mach numbers from 0.60 to 1.97 /

Title:Effects of flanges on pressure distribution on a flat plate and on a corrugated surface at mach numbers from 0.60 to 1.97 /
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Note:Washington, D.C. : National Aeronautics and Space Administration, 1974
  
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Subject:Wings (Anatomy)
Subject:Atmospheric pressure
Subject:Density altitude
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