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Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0

Title:Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0
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Note:National Aeronautics and Space Administration, 1959
  
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Subject:Airplanes -- Turbojet engines -- Afterburning
Subject:Ejector pumps
Subject:Jet nozzles
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