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Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction

Title:Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction
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Note:National Aeronautics and Space Administration ;, 1974
  
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Subject:Aerodynamics, Supersonic
Subject:Air flow
Subject:Air intakes
Subject:Airplanes -- Turbojet engines -- Air intakes
Subject:Data acquisition
Subject:Data processing
Subject:Flow geometry
Subject:Flow stability
Subject:Inlet flow
Subject:Shock waves
Subject:Supersonic flow
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