The endurance tests of the aeronautical equipment components by mathematical statistics application
Vojnotehnički Glasnik, 1998 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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Noise and performance calibration study of a Mach 2.2 supersonic cruise aircraft [PDF]
The baseline configuration of a Mach 2.2 supersonic cruise concept employing a 1980 - 1985 technology level, dry turbojet, mechanically suppressed engine, was calibrated to identify differences in noise levels and performance as determined by the ...
Maglieri, D. J., Mascitti, V. R.
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Intelligent Situational Control of Small Turbojet Engines
International Journal of Aerospace Engineering, 2018 Improvements in reliability, safety, and operational efficiency of aeroengines can be brought in a cost-effective way using advanced control concepts, thus requiring only software updates of their digital control systems.
Rudolf Andoga +6 more
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Noise measurement evaluations of various takeoff-climbout profiles of a four-engine turbojet transport airplane [PDF]
Noise measurement evaluations of various takeoff-climbout profiles of four engine turbojet transport ...
Copeland, W. L. +4 more
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Current status and opportunities for improved high-temperature materials for advanced turbojet engines [PDF]
, 1965 G. M. Ault
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Compressor noise analysis [PDF]
Prediction method for noise radiation from turbojet compressor ...
Lowson, M. V.
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Analysis of the Matching Line of between Turbine and Compressor in a Turbojet Engine
Diyala Journal of Engineering SciencesTurbojet 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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Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine
Energies, 2018 This report assesses the performance characteristics of a ramjet compression system in the application of a hypersonic vehicle. The vehicle is required to be self-powered and perform a complete flight profile using a combination of turbojet, ramjet and ...
Sasha Veeran +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.
europepmc +1 more source
Development of a turbojet combustor with a segmentally constructed liner Final summary report [PDF]
Axial and circumferential segmented combustor liners for turbojet ...
Biondi, D., Draizen, S.
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