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Determination of surge and stall limits of an axial-flow turbojet engine for control applications

Title:Determination of surge and stall limits of an axial-flow turbojet engine for control applications
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Note:National Advisory Committee for Aeronautics, 1953
  
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Subject:Aeronautics -- Research
Subject:Airplanes -- Turbojet engines
Subject:Axial flow compressors
Subject:Wind tunnel testing
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