Operating Experience With The Turbine Technologies Sr 30 Turbojet Engine Test System [PDF]
, 2020 Joseph P. Callinan, Gary Hikiss
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AerospaceSurge is a typical aerodynamic instability phenomenon in the compressors of aeroengines. The surge can lead to severe performance degradation and even structural damage to the engine and the air vehicle, making it a longstanding critical concern in the ...
Mengyang Wen +8 more
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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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RESEARCH ON APPLICATIONS OF MINI-TURBOJET AND TURBOJET ENGINED MILITARY UAVS
SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE, 2019 Mehmet TURKAY +4 more
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Transient Behavior in Variable Geometry Industrial Gas Turbines: A Comprehensive Overview of Pertinent Modeling Techniques. [PDF]
Entropy (Basel), 2021 Hashmi MB, Lemma TA, Ahsan S, Rahman S.
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Bibliography on aerodynamics of airframe/engine integration of high-speed turbine-powered aircraft, volume 1 [PDF]
This bibliography was developed as a first step in the preparation of a monograph on the subject of the aerodynamics of airframe/engine integration of high speed turbine powered aircraft.
Nichols, M. R.
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A computer program for calculating design and off-design performance for turbojet and turbofan engines [PDF]
, 1973 Program uses component performance maps to enable user to do analytical engine cycle calculations. Through scaling procedure, each of the component maps can be used to represent a family of maps.
Fishbach, L. H., Koenig, R. W.
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Investigation of the stall-induced shock wave (hammershock) at the inlet to the engine [PDF]
The peak static pressures measured at the inlet to the engine during stall are presented for a turbojet and two turbofan engines. It is shown for one turbofan and the turbojet that the static pressure ratio across the hammershock does not exceed ...
Kurkov, A. P. +2 more
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Effects of forward velocity on noise for a J85 turbojet engine with multi-tube suppressor from wind tunnel and flight tests [PDF]
, 1976 James R. Stone +2 more
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