Mixing enhancement in jet flow using the air tab technique by Wan, Chao

“…However, due to its protrusion nature, its blockage will induce thrust loss for the jet engine exhausts. This loss varies from 4.1% to 23.7% when the blockage area due to the tabs at the nozzle exit increases from 1.1% to 14.1% (Zaman (1999)). …”
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Air-film behaviour in an air-riding face seal by Ibrahim, A

“…Unlike conventional face seals, the seal must be capable of operating with moderate clearances in the order of tens to hundreds of microns and be deployable over large axial movements of several millimetres if it is to operate successfully in the jet engine environment where components are light, flexible and subject to extreme thermal growths. …”

Jet Aircrafts & Generations of Jet Fighter Aircrafts / by Madrid, Renna, author 647996

“…At these altitudes, jet engines achieve maximum efficiency over long distances. …”
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Effect of Build Parameters on the Compressive Behavior of Additive Manufactured CoCrMo Lattice Parts Based on Experimental Design by Orhan Gülcan, Ugur Simsek, Okan Cokgunlu, Mirhan Özdemir, Polat Şendur, Guney Guven Yapici

“…Due to their high specific strength, toughness, and corrosion and wear resistance characteristics, CoCrMo alloys are widely used in different industries and applications: wind turbines and jet-engine components, orthopedic implants, dental crowns, etc. …”
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Features of the application of alternative fuels in heat engines by Oleksandr Andriets, Oleh Shevchenko, Valery Ohmakevych, Mykhailo Khyzhniak

“…After analyzing the early ground test concept, the developers are planning a series of further bench tests leading to a full-scale ground test of a green hydrogen jet engine with the goal of achieving zero net carbon emissions from the engine Research Methods. …”
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A Mutual-Attention Guided Feature Extraction and Adaptative Decision Fusion Framework for Fine-Grained Dual-Band Radar Target Classification by Ao Zhong, Shiguo Chen, Tianyu Wang, Yao Ma, Yawei Zhang

“…We conducted extensive experiments on a homebrew simulated dual-band fine-grained aircraft dataset, which includes the high resolution range profile signal and the jet engine modulation signal. Compared with other classification methods, the proposed approach exhibits a remarkable classification accuracy of 95.5<inline-formula><tex-math notation="LaTeX">$\%$</tex-math></inline-formula> in our homebrew dataset and maintains an impressive accuracy of 87.4<inline-formula><tex-math notation="LaTeX">$\%$</tex-math></inline-formula> even in challenging environments with a 5 dB SNRs. …”
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Experimental determination of creep fatigue life of 316L stainless steel pipe by Mohammad, Khairul Azhar

“…Component of engineering structures operating at high temperature such as jet engine, pressure vessels, nuclear reactors, steam and gas turbine including oil and gas plant are subjected to severe thermal and mechanical loading. …”
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The development of a fixed wing aircraft analysis and design flight dynamic software by Ahmad Alaian, Ahmad Eshtiwey

“…The fourth aircraft was a jet engine aircraft while the fifth aircraft represented a turboprop aircraft. …”
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A Novel Hybrid Technique Combining Improved Cepstrum Pre-Whitening and High-Pass Filtering for Effective Bearing Fault Diagnosis Using Vibration Data by Amirmasoud Kiakojouri, Zudi Lu, Patrick Mirring, Honor Powrie, Ling Wang

“…Safran Aero Engines was the topic manager for this project) and those from three databases available in the public domain—Case Western Reserve University (CWRU), Intelligent Maintenance Systems (IMS) datasets, and Safran jet engine data—all of which have been widely used in studies of this kind. …”
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Full-Scale Turbofan Demonstration of a Deployable Engine Air-Brake for Drag Management Applications by Pfeiffer, Gordon, Davis, Rory, Hartley, Thomas, Shah, Parthiv N., Spakovszky, Zoltan S

“…The TRL-maturation effort involved design, fabrication, assembly, and ground-testing of the EAB's deployable mechanism on a full-scale, mixed-exhaust, medium-bypass-ratio business jet engine (Williams International FJ44-4A) operating at the upper end of typical approach throttle settings. …”
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Thermal control of gas turbine casings for improved tip clearance by Choi, M

“…<p>A thermal tip clearance control system provides a robust and flexible means of manipulating the closure between the casing and the rotating blade tips in a jet engine, reducing undesirable tip leakage flows. …”

Flow Management in Heat Exchanger Installations for Intercooled Turbofan Engines by Kwan, P

“…Intercooled high bypass jet engines offer a means to raise the engine pressure ratio, reduce cooling flow temperatures, reduce engine core size and thus to reduce the specific fuel consumption and increase specific power of the jet engine. …”

High pressure nozzle guide vane cooling system flow characteristics by Cresci, I

“…<p>The continuous demand from the airlines for reduced jet engine fuel consumption results in increasingly challenging high pressure turbine nozzle guide vane (NGV) working conditions. …”

Full-Scale Turbofan Demonstration of a Deployable Engine Air-Brake for Drag Management Applications by Pfeiffer, Gordon, Davis, Rory, Hartley, Thomas, Shah, Parthiv N., Spakovszky, Zoltan S

“…The TRL-maturation effort involved design, fabrication, assembly, and ground-Testing of the EAB's deployable mechanism on a full-scale, mixedexhaust, medium-bypass-ratio business jet engine (Williams International FJ44-4A) operating at the upper end of typical approach throttle settings. …”
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Development of Materials for Extreme Environment Applications by Laser Powder Bed Fusion by O'Brien, Alexander D.

“…In this study, I identify two critical advanced energy systems that may be improved with materials produced by metal additive technology, fusion reactor vacuum vessels and jet engine turbine blades, and explore the practical usage of laser powder bed fusion to improve production of relevant materials. …”
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Development of high-temperature mini ceramic gas turbine rotor by Huang, Mingyue

“…The current research focuses on fabrication and characterization of mini ceramic turbine rotor through materials design and innovation to improve fuel efficiency and reduce carbon emission of mini jet engine. A mini alumina ceramic turbine rotor has been successfully fabricated using a tailored colloidal process based on gelcasting technology. …”
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On the thermal behaviour of gas turbine filament seals by Pelegrin-Garcia, JD

“…The current life of the components is poor compared to the rest of the gas turbine, limiting the seals’ deployment, particularly in the jet engine at high temperature and pressure. Poor understanding of the seal installation response to frictional heat generated at the point of filament-rotor contact during operation has limited the ability to predict engine closures and hence seal behaviour and life. …”

Handbook of Aircraft Engines / by Alonzo, Elliot, author 646450

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Assessing selected technologies and operational strategies for improving the environmental performance of future aircraft by Mahashabde, Anuja (Anuja Anil)

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On atmospheric particulate deposition in gas turbines by Vadgama, N

“…<p>Particulate deposition has become increasingly concerning for jet engine manufacturers, it can lead to a variety of problems, from stress corrosion cracking and the blocking of cooling holes in the turbine, to reduced stall margins for the engine. …”