The endurance tests of the aeronautical equipment components by mathematical statistics application
The endurance test results of two representative components of turbojet engine are analysed using methods of mathematical statistics. The first test is related to endurance of the fuel pump, and the second one to the micropumps investigations. Researches
Dragoljub Vujić
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Optimized modeling of energy and environmental metrics of mixed flow turbofan engine used regional aircraft. [PDF]
Uçar UU, Aygun H, Tanyeri B.
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Analysis of the Matching Line of between Turbine and Compressor in a Turbojet Engine
Turbojet engines are now being given serious consideration owing to the high thrust power that they can deliver. The challenge that has arisen for the producers and designers of these engines relates to the problem of matching the compressor and the ...
Seyyed Kazem Yekani +3 more
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Smoke Diffusion Characteristics for Smoke Generator Based on Turbojet
Based on the discrete phase model in the simulation software FLUENT, the smoke diffusion characteristics under high-speed jet action of a smoke generator powered by a turbojet engine are calculated.
CAO Guangzhou, REN Rui, SUN Hongliang
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This paper covers one stress intensity factor calculation method for the blades of the turbojet.
A. E. Sheryshev, D. V. Telnov
doaj
Single Neural Adaptive PID Control for Small UAV Micro-Turbojet Engine. [PDF]
Tang W, Wang L, Gu J, Gu Y.
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Quantitative and stability study of the evolution of a thermoelastic body. [PDF]
Zinsou PH, Degla G, Ezzinbi K.
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The reliability of vibration measurements performed during turbojet engine testing depends not only on sensor accuracy but also on the configuration of the measurement system.
Roxana Nicolae +4 more
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Photographic data on the influence of the composition, preparation method, time and fuel system on the size of water droplets in a fuel-water emulsion. [PDF]
Niszczota P, Gieras M.
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Comparison of numerical simulation results of the mixing chamber with physical experiment data
The mixing chamber of a turbojet engine is the object of the study. The thermogasdynamic processes in the mixing chamber of the turbojet engine before the turbine of the turbofan attachment are the subjects of the study.
Illia Yudin
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