Evolutionary auto-design for aircraft engine cycle by Xudong Feng, Zhening Liu, Feng Wu, Handing Wang

“…Through the experimental research, new engine cycle solutions are discovered that exceed the performance of known turbojet and turbofan engines.…”
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Performance of mini jet engine combustor by Chan, Wai Lek

“…Reverse-flow combustor are normally installed on mini turbojet engines due to its smaller size and space required. …”
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Analytical Calculation Model of the TV3-117 Turboshaft Working Regimes Based on Experimental Data by Razvan Marius Catana, Gabriel Dediu

“…The experimental data were acquired from three different types of engines: TV2-117A turboshaft, AI-20K turboprop, and Viper 632-41 turbojet. The analysis method aimed to identify, through calculations, certain similarity parameters that exhibit nearly constant variations or variations within tight limits. …”
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Aircraft Target Classification Based on Correlation Features from Time-domain Echoes by Du Lan, Li Lin-sen, Li Wei-lu, Wang Bao-shuai, Shi Hui-ruo

“…This paper reports the classification of helicopters, propeller-driven aircraft, and turbojet based on differences in their time-domain modulation periods using a conventional radar system. …”
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Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor by S. L. Panchenko, T. V. Gras’ko

“…However, in this case, the use of turbojet engines operation on aviation kerosene is not possible because of the high temperatures of aircraft structural elements due to aerodynamic heating that leads to the destruction of kerosene and the impossibility of using it as fuel. …”
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Analysis of Energy Utilization and Losses for Jet-Propelled Vehicles by Mohammad Abbas, David W. Riggins

“…Example energy utilization results obtained for a modeled turbojet engine in off-design operation are provided; wake and engine component entropy generation characteristics are directly related to engine operation and flight conditions. …”
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Dynamic Design Principles of a Thrust Stand and Methods of Improving Frequency Response by Mojtaba Heydari, Amir Alaedin Motallebi, Sadegh Rahmati, Ebrahim Harirbafan

“…Successful development, evaluation, and qualification of propulsion systems such as turbojet and turbofan engines and rocket motors require the measurement of the performance and reliability of these systems. …”
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Estimation of Thrust Stand Structure Fatigue Life Under Solid Motors Random Vibrations Effects by Mojtaba Heydari, Saeed MahjoubMoghadas, Ebrahim Harirbafan, AmirAlaedin Motallebi

“…Successful development, evaluation, and qualification of propulsion systems such as turbojet and turbofan engines and rocket motors require the measurement of the performance and reliability of these systems. …”
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An Overview on Development of Small Turbine Engines for Missiles by Xue Ranran, Li Fengchao, Ren Lilei

“…To provide superior cruise thrust for high subsonic intermediate-long range missiles, small turbojet and turbofan engines have become the competitive focus for military powers. …”
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Effect of insert plate on the inlet pressure distortion of the aero-engine by Chenxin He, Zuohong Liu, Zhongyi Wang, Lei Gao, Guanglei Xu

“…This article inserts flat plate into the inlet port of a certain type of aviation turbojet engine to conduct an inlet distortion test on the entire engine. …”
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Reactivity Model as a Tool to Compare the Combustion Process in Aviation Turbine Engines Powered by Synthetic Fuels by Tomasz Białecki, Wojciech Dzięgielewski, Mirosław Kowalski, Andrzej Kulczycki

“…Bench tests were carried out on a test rig with a miniature turbojet engine, according to authorial methodology. …”
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Simulating aero-engine performance and emissions characteristics running on green diesel by Altarazi, Yazan S. M., Abu Talib, Abd. Rahim, Yu, Jianglong, Gires, Ezanee, Abdul Ghafir, Mohd Fahmi, Lucas, John, Yusaf, Talal

“…This study aims to run a Kingtech K-180 turbojet engine using green diesel fuel (produced of waste cooking oil through a deoxygenating process) and its blend. …”

ASSESSING EXPORT COMPETITIVENESS IN THE CONTEXT OF GROWTH IN EMERGING ECONOMIES. THE EXAMPLE OF UKRAINE by Oleh Pustovoit

“…These include: insulated wires, cables and other insulated electrical conductors; fiber optic cables; turbojet engines, turboprops and other gas turbines; electric heating appliances and devices; parts of aircraft. …”
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CFD simulations on the compressor of a mini-jet engine- II by Low, Bin Bin.

“…Efforts have thus been made to miniaturise turbojet engines for UAV applications. This project aims to establish a Computational Fluid Dynamics (CFD) simulation framework for the SR-30 mini jet engine compressor to better understand the flow within a miniaturised centrifugal compressor. …”
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Extreme Learning Machine-Based Diagnostics for Component Degradation in a Microturbine by Nicola Menga, Akhila Mothakani, Maria Grazia De Giorgi, Radoslaw Przysowa, Antonio Ficarella

“…Micro turbojets are used for propelling radio-controlled aircraft, aerial targets, and personal air vehicles. …”
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Power Balance Strategies in Steady-State Simulation of the Micro Gas Turbine Engine by Component-Coupled 3D CFD Method by Yibing Xu, Lei Gao, Ruizhe Cao, Chong Yan, Ying Piao

“…By carrying out the ‘component-matched’ simulation and the ‘component-coupled’ simulation for a micro turbojet engine, the necessity of introducing the power balance iteration was discussed in this paper. …”
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High Temperature Magnetic Sensors for the Hot Section of Aeroengines by Edward Rokicki, Radoslaw Przysowa, Jerzy Kotkowski, Paweł Majewski

“…Moreover, a set of six probes passed an initial engine test in an SO-3 turbojet. It was confirmed that the proposed design of the inductive sensor is suitable for blade health monitoring (BHM) of the last stages of compressors and gas turbines operating below 1000 °C, even without a dedicated cooling system. …”
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Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle by Yu. V. Zinenkov, A. V. Lukovnikov, S. V. Agaverdyev

“…The process of conducting optimization studies of the Unmanned aerial vehicle power plant system with a bypass turbojet engine with mixing of the circuit flows behind the turbine is described. …”
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Design, Numerical and Experimental Investigation of High Swirling Flow in an Annular Combustion Chamber by Zahra Ghahramani, Masoud Zareh, Hossein Pourfarzaneh, Farshad Pazooki

“…In this study, an annular combustion chamber of a turbojet engine with a net trust of 1650N is designed. …”
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Influence of Gaseous Hydrogen Addition on Initiation of Rotating Detonation in Liquid Fuel–Air Mixtures by Jan Kindracki, Krzysztof Wacko, Przemysław Woźniak, Stanisław Siatkowski, Łukasz Mężyk

“…It is an excellent fuel for thermal engines: piston, turbojet, rocket, and, going forward, in thermonuclear power plants. …”
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