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Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0

Title:Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0
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Note:National Advisory Committee for Aeronautics, 1956
  
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Subject:Aerodynamics, Supersonic
Subject:Air ducts
Subject:Airplanes -- Wings
Subject:Mach number
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