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Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude

Title:Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
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Note:National Aeronautics and Space Administration Scieentific and Technical Information Branch ;, 1983
  
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Subject:Airplanes -- Flight testing
Subject:Airplanes -- Motors -- Thrust
Subject:Airplanes -- Turbojet engines
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