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Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds

Title:Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
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Note:National Advisory Committee for Aeronautics, 1958
  
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Subject:Aerodynamics, Supersonic
Subject:Aerodynamics, Transonic
Subject:Air ducts
Subject:Air flow
Subject:Airplanes -- Turbojet engines -- Air intakes
Subject:Charts, diagrams, etc.
Subject:Mathematics
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