Relevant bibliographies by topics / Jet engine

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Jet engine'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Jet engine"

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Chen, Ruiyang. "Advanced development and future of jet engines." Theoretical and Natural Science 12, no. 1 (2023): 162–66. http://dx.doi.org/10.54254/2753-8818/12/20230457.

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An aerodynamic reaction engine, a jet engine, is an internal combustion engine that produces thrust through jet thrust. A jet engine is an important power unit used in aviation and spaceflight, which generates thrust by pushing air in reverse. In recent decades, various developments and improvements have significantly enhanced the efficiency and performance of jet engines. These engines are divided into turbojets, turbojets, turboprops, turboshafts, and ramjets. This article will begin with an introduction to the different types of jet engines and then detail the design, benefits, and issues o
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Liu, Hangyu. "Current Status of Jet Engines and Their future." Highlights in Science, Engineering and Technology 43 (April 14, 2023): 280–86. http://dx.doi.org/10.54097/hset.v43i.7430.

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Jet engines have important application value and status in the aerospace field, which directly affects the development of aircraft and spacecraft. This year, jet engines have gradually become the focus and hotspot of scholars at home and abroad. Through the method of literature comparison and analysis, this paper focuses on analysing two common jet engines, namely turbofan engine and pulse jet engine, and makes a detailed analysis and comparison of their working principles and applications; for the future development of parts, three-dimensional (3D) printing technology as an example, the use o
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Langston, Lee S. "For Jet Engine Wing Mounting." Mechanical Engineering 140, no. 09 (2018): S52—S53. http://dx.doi.org/10.1115/1.2018-sep4.

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The mounting of a jet engine under the wing of an airliner can be a daunting task for turbofan engineers. Thrust forces generated by gas path momentum flow changes in a jet engine are transmitted by pressure (and friction) forces on stators and struts attached to the engine case. Case engine mounts then transmit the thrust forces (as high as 100,000 pounds thrust on the largest engines) to the wing pylons to pull the plane forward. The mounts must also support the engine weight (as high as 20,000 pounds) and carry nacelle flight loads. Engine bypass ratios are increasing (12:1 on the new geare
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Saitoh, K., A. Fushimi, S. Matsuyama, et al. "Elemental analysis of aircraft engine smoke number filter samples with micro-PIXE." Journal of Physics: Conference Series 2326, no. 1 (2022): 012002. http://dx.doi.org/10.1088/1742-6596/2326/1/012002.

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Abstract To extract information on elemental components and PM characteristics from smoke number (SN) filter paper, we were performed elemental analysis by micro-PIXE. As a result of elemental analysis of the SN filter, information on the elemental composition of jet engine exhaust PM was obtained. Regarding the SN filter, jet engine exhaust PM have been collected for each difference in engine thrust of various aircraft engines at aircraft turbine engines test cells around the world. By periodically analyzing the elemental composition of such the SN filter, it is possible to grasp the characte
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Hu, Lichen, Feiyu Long, Borui Xie, and Xuanzhou Zhuang. "Four variants of turbofan, turbojet, turboprop and ramjet engines and their future prospects." Applied and Computational Engineering 11, no. 1 (2023): 137–42. http://dx.doi.org/10.54254/2755-2721/11/20230222.

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A jet engine is a sophisticated machine that has revolutionized the aviation industry. It is a type of internal combustion engine that uses air as its oxidizer and fuel to produce thrust. The third law of motion, which states that there is an equivalent and opposite response to every action, governs how the engine functions. Compressed air is combined with fuel, ignited in the combustion chamber, and then expelled out of the jet engine at a high rate of speed to create propulsion. The development of jet engines has been a long and arduous process, with many different designs and configurations
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Gusev, Evgeniy V., Vladimir A. Zagovorchev, Vladimir V. Rodchenko, Elnara R. Sadretdinova, and Elizaveta A. Shipnevskaya. "Calculation of the parameters and characteristics of a rotating lunar jet penetrator." Siberian Aerospace Journal 24, no. 4 (2023): 706–16. http://dx.doi.org/10.31772/2712-8970-2023-24-4-706-716.

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The purpose of the work is to determine the parameters of the internal ballistics of a solid fuel jet engine mounted on a jet penetrator entering the ground at a high rotation speed around its own axis. Research methods: to determine the pressure in the chamber of a rotating engine, the known equations for the balance of gas inflow and consumption are usually used, as in the case of a non-rotating solid fuel jet engine. The difference between the internal ballistics of a rotating solid fuel jet engine is that the effect of rotation on the operating process is taken into account by the coeffici
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Pismennyi, V. L. "Hyper Afterburner Jet Engines." Proceedings of Higher Educational Institutions. Маchine Building, no. 01 (718) (January 2020): 51–62. http://dx.doi.org/10.18698/0536-1044-2020-1-51-62.

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This paper introduces a thrust augmentation method for super- and hypersonic jet engines by means of applying water at the engine intake. This method expands the use of jet engines with subsonic combustion, allowing velocities up to Mach 8 and altitude up to 45 km. At velocities higher than 3–4 Mach, stagnation temperature of the air is getting higher than the critical temperature of water, which makes the existence of water at the gas turbine engine intake impossible. Water vapour as a working medium of a jet engine creates the so-called inner thermodynamic circle. This phenomenon defines the
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Chachurski, Ryszard, Łukasz Omen, Andrzej J. Panas, and Piotr Zalewski. "Mobile engine test station for preparation and operation of miniature turbine jet engines for flying aerial targets." Bulletin of the Military University of Technology 69, no. 4 (2020): 57–72. http://dx.doi.org/10.5604/01.3001.0015.3819.

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The work presents description and operation of the mobile engine test station, designed for the miniature turbine jet engines with a maximum trust below 200 N. The engine test bed allows us to monitor the condition of the engine used to drive remotely controlled flying aerial targets or military unmanned aircraft. According to military (Department of Defence) requirements, the designed engine test station is mobile, it can be used in military battlefield conditions and it meets safety precautions and military transport requirements. The reason of the engine investigations was the shortage and
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Garwol, Arkadiusz. "Jet engine - construction and modern development examples." Technologia i Automatyzacja Montażu 125, no. 3 (2024): 38–43. http://dx.doi.org/10.7862/tiam.2024.3.5.

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The article presents the construction and operating principle of a turbine jet engine. The basic types of engines of this type are presented, such as single-rotor single-flow jet engines, single-flow dual-rotor engines (which are another development version of single-rotor engines, as well as dual-flow engines which are currently most commonly used in passenger aviation, and contra-rotating propeller engines and turbine propeller engines. Also presented their applications, such as propulsion of various types of. In the further part of this paper, the development trends of turbine jet engines a
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Fan, Chengye, Ruoshui Jiang, and Songzhi Zhang. "Current Status and Future Prospects of Jet Engines." Highlights in Science, Engineering and Technology 29 (January 31, 2023): 240–46. http://dx.doi.org/10.54097/hset.v29i.4836.

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Current status and future prospects of Jet engine are described in this paper. Specifically, this paper contains three aspects: the current application of jet engines, the advantages and disadvantages of four major types of jet engines, and its future development trends. The method of the paper is analyze main four types of Jet Engines principle separately, and makes comparisons. Specifically, those four main types of Jet Engines are turbojet, turbofans, turboprops and ramjets. Moreover, if people want to understand Jet Engines, understand how Brayton cycle run is necessary. Brayton cycle is t
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Dissertations / Theses on the topic "Jet engine"

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Joo, Won-Gu. "Intake/engine flowfield coupling in turbofan engines." Thesis, University of Cambridge, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.319865.

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Kundu, Reema. "Impact of engine icing on jet engine compressor flow dynamics." Diss., Georgia Institute of Technology, 2015. http://hdl.handle.net/1853/54870.

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Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This previously unrecognized form of icing occurs in flights through high altitude convective regions and vicinity of thunderstorms. Engine icing events involve power loss or damage associated to the engine core, namely instabilities such as compressor surge, stall, engine rollback and even combustor flameout events. The effects on compressor performance are significant in understanding the response of the engine to atmospheric ice ingestion. A one-dimensional axisymmetric flow model is used to simulate
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Gilmore, Jordan David. "Computational Fluid Dynamics Analysis of Jet Engine Test Facilities." Thesis, University of Canterbury. Mechanical Engineering, 2012. http://hdl.handle.net/10092/7238.

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This thesis investigates the application of CFD techniques to the aerodynamic analysis of a U-shaped JETC. Investigations were carried out to determine the flow patterns present at a number of locations within the structure of a full U-shaped JETC. The CFD solutions produced in these investigations used recommendations from the literature in the set-up of the CFD solver, and provided the computational component towards problem-specific validation of the CFD techniques used. A structured series of CFD-aided investigation and design processes were then performed. These processes were based aro
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Kareliusson, Joakim, and Melker Nordqvist. "Conceptual Design of a Supersonic Jet Engine." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-26067.

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This thesis is a response to the request for proposal issued by a joint collaboration between the AIAA Foundation and ASME/IGTI as a student competition to design a new turbofan engine intended for a conceptual supersonic business jet expected to enter service in 2025. Due to the increasing competition in the aircraft industry and the more stringent environmental legislations the new engine is expected to provide a lower fuel burn than the current engine intended for the aircraft to increase the chances of commercial success. The thesis has one main and one secondary objective, the main object
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Sides, Steve P. (Steve Paul) 1963. "Driving robust jet engine design through metrics." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/88331.

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Soucy, Arthur L. "De-commoditizing the commercial jet engine business." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/39517.

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Thesis (M.B.A.)--Massachusetts Institute of Technology, Sloan School of Management, 2007.<br>Includes bibliographical references.<br>This thesis project is a comprehensive application of the Delta Model at a major jet engine manufacturer. It will assess and contrast customer segmentation and customer value proposition via primary research. It will also assess and contrast the current and future state "bundle of competencies" within the firm. Utilizing the frameworks of the Delta Model, we will then define the mission of the business and the strategic agenda. Once these are understood we will d
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Gnanakumaran, Gnanach Selvan. "Condensation in jet engine intakes and fans." Thesis, University of Cambridge, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.609623.

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KAMARAJ, JAYACHANDRAN. "MODELING AND SIMULATION OF SINGLE SPOOL JET ENGINE." University of Cincinnati / OhioLINK, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1073935505.

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Seal, David A. (David Allen). "Fault tolerant issues in jet engine compressor control." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/44277.

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Erickson, Robert R. "A numerical investigation on the influence of engine shape and mixing processes on wave engine performance." Available online, Georgia Institute of Technology, 2005, 2004. http://etd.gatech.edu/theses/available/etd-01032005-100101/unrestricted/erickson%5Frobert%5Fr%5F200505%5Fphd.pdf.

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Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2005.<br>Ben T. Zinn, Committee Chair ; Jeff Jagoda, Committee Member ; Suresh Menon, Committee Member ; Tim Lieuwen, Committee Member ; Rick Gaeta, Committee Member. Vita. Includes bibliographical references.
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Books on the topic "Jet engine"

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Rolls-Royce, ed. The Jet engine. 4th ed. Rolls-Royce, 1986.

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W, Awdry. Thomas, and the jet engine. Egmont, 2011.

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ill, Courtney Richard, and Awdry W, eds. Thomas and the jet engine. Random House Children's Books, 2009.

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B, Murthy S. N., United States. National Aeronautics and Space Administration., and United States. Federal Aviation Administration., eds. Jet engine simulation with water ingestion through compressor. National Aeronautics and Space Administration, 1987.

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Haught, Dan. Microsoft Jet database engine programmer's guide. 2nd ed. Microsoft Press, 1997.

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Thompson, Haydn A. Parallel Processing for Jet Engine Control. Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1972-2.

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Weber, H. E. Shock wave engine design. Wiley, 1995.

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M, Hernan, Sarohia V, Federal Aviation Administration Technical Center (U.S.), and Jet Propulsion Laboratory (U.S.), eds. Quantitative determination of engine water ingestion. U.S. Dept. of Transportation, FAA Technical Center, 1986.

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United States. National Aeronautics and Space Administration., ed. Euler solutions for an unbladed jet engine configuration. National Aeronautics and Space Administration, 1991.

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United States. National Aeronautics and Space Administration, ed. Advanced smoke meters for jet engine exhaust measurement. National Aeronautics and Space Administration, 1986.

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Book chapters on the topic "Jet engine"

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Decher, Reiner. "The Compressor: Gas Turbine Engine Keystone." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_10.

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AbstractAll engines involve the raising of pressure in the engine’s medium, be it liquid compression of water, piston-cylinder compression of air or compression by aerodynamic forces. The last is the hardest because it is required to be efficient and stable. An aerodynamic air compressor works by slowing velocities to raise pressure. The airfoil has a difficult time doing this reliably and well and so does the compressor. When it does, it allows for amazing performance of the engine in terms of power and efficiency.
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Decher, Reiner. "More Components: Inlets, Mixers, and Nozzles." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_13.

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AbstractTheintegrationof a gas turbine engine into a functioning jet propulsion engine for an airplane requires more components: inlets and nozzles. For the inlet, the special care exercised to avoid ingestion of boundary layers air is described. The design features of nozzles are described and extended to include discussion of more extreme configurations such as those found on rocket engines.
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Decher, Reiner. "Propulsion for Flight: Power or Thrust?" In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_9.

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AbstractAn engine is required to provide the power necessary for overcoming the drag of flight. There are not many engine types available to perform that important function: they all have advantages and limitations. They share common features and are different in fundamental ways. The histories of their development paced the history of man’s ability to fly and the modern gas turbine engine is the climax of that progression toward today’s state of aviation. In this chapter we focus on the salient features of engines as they relate to flight.
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Hazlett, Robert N., and James M. Hall. "Jet Aircraft Fuel System Deposits." In Chemistry of Engine Combustion Deposits. Springer US, 1985. http://dx.doi.org/10.1007/978-1-4613-2469-0_13.

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Armanidis, Konstantinos, Sebastian Kurth, Viet Nghiem, and Joerg R. Seume. "Exhaust Jet Analysis." In Regeneration of Complex Capital Goods. Springer International Publishing, 2024. http://dx.doi.org/10.1007/978-3-031-51395-4_4.

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AbstractThe aim of project A3 of the Collaborative Research Centre (CRC) 871 is to develop a novel method for automated condition assessment of aircraft engines. The method is based on a combination of numerical simulations, Background Oriented Schlieren (BOS) measurements, and the use of pattern recognition algorithms. The density distribution in the exhaust gas stream of the engine is first measured using the BOS method and then compared with a damage library which was generated numerically through CFD. The automated classification of damage cases can be realized using pattern recognition al
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Decher, Reiner. "Other Components of the Jet Engine." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_12.

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AbstractThecompressor may be the challenging component of a gas turbine engine, a combustor and a turbine also must function efficiently. The design aspects of these two components are described here together with how the engine is configured and works as a system.
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Thompson, Haydn A. "Controller and Engine Simulation Implementation." In Parallel Processing for Jet Engine Control. Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1972-2_2.

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Ayyappan, Dhanesh, Aravind Vaidyanathan, C. K. Muthukumaran, and K. Nandakumar. "Study of Instability Nature of Circular Liquid Jet at Critical Chamber Conditions." In Advanced Engine Diagnostics. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-3275-3_10.

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Thompson, Haydn A. "Preliminaries." In Parallel Processing for Jet Engine Control. Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1972-2_1.

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Thompson, Haydn A. "Controller and Engine Simulation Implementation on the Inmos Transputer." In Parallel Processing for Jet Engine Control. Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1972-2_3.

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Conference papers on the topic "Jet engine"

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Abu-Hakima, Suhayya, Philippe Davidson, Mike Halasz, and Sieu Phan. "Jet engine technical advisor (JETA)." In the second international conference. ACM Press, 1989. http://dx.doi.org/10.1145/66617.66637.

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MEISL, CLAUS. "Rocket engine versus jet engine comparison." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3686.

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Kato, Naoto, Shunsuke Watanabe, and Hiroaki Hasegawa. "Experimental Study of Aerodynamic Drag Control on Bluff Body using Synthetic Jets." In Small Engine Technology Conference & Exposition. Society of Automotive Engineers of Japan, 2020. http://dx.doi.org/10.4271/2019-32-0538.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;Since flow separation causes increase of the drag on bluff bodies, its control method has been studied for many years. Active control methods are currently focused as an alternative to passive ones because they impose a larger drag penalty under certain conditions. Although the effectiveness of a steady jet using suction, blowing or pulsed jets has been demonstrated, it is difficult to obtain an effect commensurate with weight increase because the mechanism is complicated.&lt;/div&gt;&lt;div class="htmlview paragraph"&gt
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Chiang, Richard, Fred Hadaegh, and C. Lin. "Robust jet engine control." In Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-3927.

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Bacon, Richard, and Jan Roskman. "The 3X jet - An advanced engine configuration for two-engine jet aircraft." In Aircraft Engineering, Technology, and Operations Congress. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-3963.

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Yoshida, Koji, Hideo Shoji, and Hidenori Tanaka. "Performance of Newly Developed Plasma Jet Igniter." In Small Engine Technology Conference & Exposition. SAE International, 1999. http://dx.doi.org/10.4271/1999-01-3327.

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Taghavi, Ray, and Saeed Farokhi. "Using Jet Engine Simulator in Propulsion Education." In ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/ajkfluids2019-4963.

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Abstract Undergraduate education in jet propulsion can benefit from a modern real-engine simulator. The traditional lecture/laboratory course in propulsion continues to emphasize fundamental aerothermodynamics and often includes a propulsion laboratory that tests small engines (e.g., micro-turbojet engines) mounted on a thrust stand. Modern engine simulators, as virtual test bench, offer new tools and capabilities that help students learn the fundamentals as well as jet engine response to dynamic throttle setting. Geared, high-bypass ratio, two-spool turbofan engines can be simulated in a virt
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MOREY, WILLIAM W. "Jet engine combustor viewing system." In Conference on Lasers and Electro-Optics. OSA, 1985. http://dx.doi.org/10.1364/cleo.1985.fo1.

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Bacon, Richard, and Jan Roskam. "The 3x Jet Engine Configuration." In General, Corporate & Regional Aviation Meeting & Exposition. SAE International, 1995. http://dx.doi.org/10.4271/951173.

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FISHER, MJ, and BJ TESTER. "JET ENGINE NOISE SOURCE BREAKDOWN." In Noise Source Location 1981. Institute of Acoustics, 2024. http://dx.doi.org/10.25144/23192.

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Reports on the topic "Jet engine"

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Kodres, C. A. Jet Engine Test Cell Noise Reduction. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada380948.

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Prasad, J. V., and Carlos Rivera. Broad-Based High Frequency Jet Engine Control. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada311100.

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Nowlin, Jacob, Kevin Wallace, Kyle Beurlot, Mark Patterson, and Timothy Jacobs. PR-457-21206-R01 CFD Study of Prechamber NOx Production Mechanisms. Pipeline Research Council International, Inc. (PRCI), 2023. http://dx.doi.org/10.55274/r0000027.

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Use of the pre-combustion chamber (PCC) as an ignition source in large-bore natural gas engines has shown promise in reducing emissions. By increasing the ignition energy and surface area via a turbulent jet, these devices can extend the lean operating limit of the engine and reduce oxides of nitrogen (NOx). This study aims to characterize the sensitivity of main chamber NOx formation to changes in the PCC jet. A CFD model of a Cooper-Bessemer GMV two-stroke lean-burn natural gas engine is used for this purpose. The temperature and chemical composition of the PCC jet are varied across several
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Shumway, L. A. Characterization of Jet Engine Exhaust Particulates for the F404, F118, T64, and T58 Aircraft Engines. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada405470.

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Wurtzler, Kenneth, Amid Ansari, and Don Kinsey. Computational Fluid Dynamic Analysis of a Single-Engine Business Jet. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada332966.

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Shumway, L. A. Trace Element and Polycyclic Aromatic Hydrocarbon Analyses of Jet Engine Fuels: Jet A, JP5, and JP8. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada390641.

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Alba, Patricia A., and Herbert G. Baker. Job Performance Measurement Package for the J-79 Jet Engine Mechanic. Defense Technical Information Center, 1988. http://dx.doi.org/10.21236/ada199568.

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Kuprowicz, Nicholas J. The Integrated Multi-Objective Multi-Disciplinary Jet Engine Design Optimization Program. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada372032.

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Schumacher, Phillip M. Characterization of Aerosols from JP-8 Fuels in Jet Engine Emissions. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada374730.

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Kinkead, E. R., S. R. Bunger, R. E. Wolfe, and H. G. Wall. The Acute, Delayed Neurotoxicity Evaluation of Two Jet Engine Oil Formulations. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada222018.

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