Emission calibration of a J-58 afterburning turbojet engine at simulated supersonic stratospheric flight conditions [PDF]
Emissions of total oxides of nitrogen, unburned hydrocarbons, and carbon monoxide from a J-58 engine at simulated flight conditions of Mach 2.0, 2.4, and 2.8 at 19.8 km altitude are reported.
Holdeman, J. D.
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CENTRIFUGAL COMPRESSOR HEAD CHARACTERISTIC OF A MICRO TURBOJET ENGINE BASED ON NUMERICAL SIMULATION
Bestoon Najmuldeen Abdullah Abdullah +2 more
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Transient Behavior in Variable Geometry Industrial Gas Turbines: A Comprehensive Overview of Pertinent Modeling Techniques. [PDF]
Hashmi MB, Lemma TA, Ahsan S, Rahman S.
europepmc +1 more source
Summary of recent investigations of inlet flow distortion effect on engine stability [PDF]
A review is presented of recent experimental results, analytical procedures and test techniques employed to evaluate the effects of inlet flow distortion on the stability characteristics of representative afterburning turbofan and turbojet compression ...
Braithwaite, W. M., Graber, E. J., Jr.
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Near Magnetic Field of a Small Turbojet Engine
Rudolf Andoga, Ladislav Fözö
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Environmental and High-Strain Rate effects on composites for engine applications [PDF]
The Lewis Research Center is conducting a series of programs intended to investigate and develop the application of composite materials to structural components for turbojet engines.
Chamis, C. C., Smith, G. T.
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A turbojet simulator for Mach numbers up to 2.0 [PDF]
A turbojet simulator was designed and fabricated for use in wind tunnel models. The simulator contains a six-stage, axial-flow compressor powered by a three-stage, axial-flow turbine. High pressure heated air was used to drive the turbine.
Nosek, S. M. +3 more
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Experimental and numerical studies of the design of statically indeterminate turbojet engines [PDF]
Paweł Bałon +3 more
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CFD simulation of updrafts initiated by a vertically directed jet fed by the heat of water vapor condensation. [PDF]
Abshaev MT +7 more
europepmc +1 more source
Application of binary programming to turbojet engine fault detection
C A. BOTSARIS +2 more
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