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The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23° conical-diffuser-tail-pipe combination

Title:The effect of the inlet mach number and inlet-boundary-layer thickness on the performance of a 23° conical-diffuser-tail-pipe combination
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Note:National Advisory Committee for Aeronautics, 1950
  
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Subject:Boundary layer
Subject:Cone -- Aerodynamics
Subject:Diffusers -- Aerodynamics
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