Self-teaching digital-computer program for fail-operational control of a turbojet engine in a sea-level test stand [PDF]
The design and evaluation are described of a digital turbojet engine control which is capable of sensing catastrophic failures in either the engine rotor speed or the compressor discharge static-pressure signal and is capable of switching control modes ...
Arpasi, D. J., Wallhagen, R. E.
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Numerical investigation of a GTM-140 turbojet engine
Open Engineering, 2015 The paper presents three-dimensional numerical simulations of combustion in the GTM-140 miniature turbine engine. The main aim of the work is to understand the processes occurring in the combustion chamber.
Suchocki Tomasz +2 more
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Optimized modeling of energy and environmental metrics of mixed flow turbofan engine used regional aircraft. [PDF]
J Therm Anal Calorim, 2023 Uçar UU, Aygun H, Tanyeri B.
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Experimental investigation of cermet turbine blades in an axial-flow turbojet engine [PDF]
, 1958 William C. Morgan, G. C. Deutsch
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Comprehensive Review of Emerging Missile Propulsion Technologies [PDF]
Hangkong bingqiPower system is a core factor influencing the performance of tactical missile. As conventional propulsion system, solid-rocket engine, turbojet engine, and sub-sonic combustion ramjet engines have become increasingly mature, and the technological ...
Ma Conghui, Shen Xin, Qin Fei, Sun Zhenhua
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Turbine for ordnance turbojet engine. 2: Cold-air performance with opened stator [PDF]
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throat area on the performance level of a turbojet engine turbine.
Haas, J. E. +2 more
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Turbojet and turbofan engines for a mach 3 supersonic transport [PDF]
, 1964 James Dugan +3 more
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Effects of chemical equilibrium on turbine engine performance for various fuels and combustor temperatures [PDF]
A study was performed to quantify the differences in turbine engine performance with and without the chemical dissociation effects for various fuel types over a range of combustor temperatures.
Snyder, Christopher A., Tran, Donald H.
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Engineering Transactions, 1991 The relations are derived enabling to estimate the acceleration time of the turbojet engine rotor set. The terms are established allowing for the determination of the effect of individual operational and structural engine parameters upon the time needed
M. Orkisz
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Single Neural Adaptive PID Control for Small UAV Micro-Turbojet Engine. [PDF]
Sensors (Basel), 2020 Tang W, Wang L, Gu J, Gu Y.
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