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Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Title:Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8
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Note:National Advisory Committee for Aeronautics, 1951
  
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Subject:Charts, diagrams, etc.
Subject:Drag (Aerodynamics)
Subject:Jet engines -- Air intakes
Subject:Noses (Aircraft)
Subject:Pressure
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