参见、参考文献、外部链接:涡轮风扇发动机
本文为辽观整合的中英文词条的参见、参考文献、外部链接部分。
参见、参考文献、外部链接
Wikipedia; CathayVista
8/25/20245 min read
1. 参见(维基百科的相关词条)
提示:本部分链接中有些指向无法从中国内地直接访问的站点。
Variable cycle engine 变循环发动机
Turbine engine failure 涡轮发动机故障
Gas turbine 燃气轮机
Axial fan design 轴流风机设计
2. 英文词条参考文献
提示:本部分链接中有些指向无法从中国内地直接访问的站点。
注:由于中文词条未列出参考文献,本部分仅包括英文词条的引用列表。
· Marshall Brain (April 2000). "How Gas Turbine Engines Work". howstuffworks.com. Retrieved 2010-11-24.
· Hall, Nancy (May 5, 2015). "Turbofan Engine". Glenn Research Center. NASA. Retrieved October 25, 2015. Most modern airliners use turbofan engines because of their high thrust and good fuel efficiency.
· Michael Hacker; David Burghardt; Linnea Fletcher; Anthony Gordon; William Peruzzi (March 18, 2009). Engineering and Technology. Cengage Learning. p. 319. ISBN 978-1-285-95643-5. Retrieved October 25, 2015. All modern jet-powered commercial aircraft use high bypass turbofan engines [...]
· Verma, Bharat (January 1, 2013). Indian Defence Review: Apr–Jun 2012. Lancer Publishers. p. 18. ISBN 978-81-7062-259-8. Retrieved October 25, 2015. Military power plants may be divided into some major categories – low bypass turbofans that generally power fighter jets…
· Frank Northen Magill, ed. (1993). Magill's Survey of Science: Applied science series, Volume 3. Salem Press. p. 1431. ISBN 9780893567088. Most tactical military aircraft are powered by low-bypass turbofan engines.
· Thrust Augmentation with Mixer/Ejector systems,Presz,Reynolds,Hunter,AIAA 2002-0230,p.3
· Gas Turbine Aerothermodynamics With Special Reference To Aircraft propulsion,Sir Frank Whittle 1981,ISBN 0 08 026719 X, p.217
· Gas Turbine Aerothermodynamics With Special Reference To Aircraft propulsion,Sir Frank Whittle 1981,ISBN 0 08 026719 X, p.218
· Rubert, Kennedy F. (1945-02-01). "An analysis of jet-propulsion systems making direct use of the working substance of a thermodynamic cycle": 2–3.
· Roth, Bryce Alexander (2000-09-01). A theoretical treatment of technical risk in modern propulsion system design (Thesis). Bibcode:2000PhDT.......101R. p.76
· Journal of Aircraft September-October 1966: Vol 3 Iss 5. Internet Archive. American Institute of Aeronautics and Astronautics. September 1966. p. 386.
· Journal of Aircraft September-October 1966: Vol 3 Iss 5. Internet Archive. American Institute of Aeronautics and Astronautics. September 1966. p. 387.
· "Bypass ratio", Britannica
· Thermodynamics, MIT, archived from the original on 2013-05-28
· Jet Propulsion, Nicholas Cumpsty 2003,ISBN 978 0 521 54144 2, Figure 7.3 Predicted variation in thrust and sfc with bypass ratio for a constant core
· "Practical considerations in designing the engine cycle", M G Philpot, AGARD LS 183,Steady and Transient Performance Prediction,ISBN 92 835 0674 X, p.2-12
· "Flight global" (PDF). Flightglobal.com.
· Taylor, John W.R. (ed.), All The World's Aircraft 1975–1976, Paulton House, 8 Sheperdess Walk, London N1 7LW: Jane's, p. 748
· Proceedings, ASME, 15 April 2015, doi:10.1115/84-GT-230
· "PW tales", Road runners Internationale
· "Turbofan Engine". GRC NASA. Retrieved 2010-11-24.
· Neumann, Gerhard (2004) [first published by Morrow 1984]. Herman the German: Just Lucky I Guess. Bloomington, Indiana, US: Authorhouse. pp. 228–30. ISBN 1-4184-7925-X.
· "The turbofan engine" Archived 2015-04-18 at the Wayback Machine, p. 7. SRM Institute of Science and Technology, Department of Aerospace Engineering.
· Cohen; Rogers; Saravanamuttoo (1972). Gas Turbine Theory (2nd ed.). Longmans. p. 85. ISBN 0-582-44927-8.
· FAA-H-8083-3B Airplane Flying Handbook Handbook (PDF). Federal Aviation Administration. 2004. Archived from the original (PDF) on 2012-09-21.
· "Turbofan Thrust". Grc.nasa.gov. Retrieved 1 March 2022.
· Goulos, Ioannis; Stankowski, Tomasz; MacManus, David; Woodrow, Philip; Sheaf, Christopher (February 2018). "Civil Turbofan Engine Exhaust Aerodynamics: Impact of Bypass Nozzle After-body Design" (PDF). Aerospace Science and Technology. 73: 85–95. doi:10.1016/j.ast.2017.09.002. hdl:1826/12476. Retrieved 1 March 2022.
· Kempton, A., "Acoustic liners for modern aero-engines", 15th CEAS-ASC Workshop and 1st Scientific Workshop of X-Noise EV, 2011. Win.tue.nl.
· Smith, Michael J. T. (19 February 1970). "Softly, softly towards the quiet jet". New Scientist. fig. 5.
· Kester, JD; Slaiby, TG (1968). "Designing the JT-9D Engine to meet Low Noise Requirements for Future Transports". SAE Transactions. 76 (2): 1332. doi:10.4271/670331. JSTOR 44565020. paper 670331.
· Smith, M.J.T. (17 August 1972). "Quiet Propulsion". Flight International. p. 241.
· McAlpine, A., Research project: Buzz-saw noise and nonlinear acoustics, University of Southampton
· Schuster, B.; Lieber, L.; Vavalle, A. (2010), "Optimization of a seamless inlet liner using an empirically validated prediction method", 16th AIAA/CEAS Aeroacoustics Conference, Stockholm, SE, doi:10.2514/6.2010-3824, ISBN 978-1-60086-955-6, S2CID 113015300
· Ferrante, P. G.; Copiello, D.; Beutke, M. (2011), "Design and experimental verification of 'true zero-splice' acoustic liners in the universal fan facility adaptation (UFFA) modular rig", 17h AIAA/CEAS Aeroacoustics Conference, Portland, OR, doi:10.2514/6.2011-2728, ISBN 978-1-60086-943-3, AIAA-2011-2728
· Banke, Jim (2012-12-13). "NASA Helps Create a More Silent Night". NASA. Retrieved January 12, 2013.
· Zaman, K. B. M. Q.; Bridges, J. E.; Huff, D. L. (17–21 December 2010). "Evolution from 'Tabs' to 'Chevron Technology'–a Review" (PDF). Proceedings of the 13th Asian Congress of Fluid Mechanics 17–21 December 2010, Dhaka, Bangladesh. Cleveland, OH: bNASA Glenn Research Center. Retrieved January 29, 2013.
· "Invited" (PDF), 13th ACFM, CN: AFMC, archived from the original (PDF) on 2014-03-25
· "Turbojet History And Development 1930–1960 Volume 1", The Crowood Press Ltd. 2007, ISBN 978 1 86126 912 6, p. 241.
· "Metrovick F3 Cutaway – Pictures & Photos on FlightGlobal Airspace". Flightglobal.com. 2007-11-07. Retrieved 2013-04-29.
· "page 145". Flight international. 1946.
· "1954 | 0985 | Flight Archive". Flightglobal.com. 1954-04-09. Retrieved 2013-04-29.
· The Development Of Jet And Turbine Aero Engines 4th edition, Bill Gunston 2006, ISBN 0 7509 4477 3, p. 197.
· Boyne, Walter J., ed. (2002). Air warfare: An international encyclopedia: A–L. ABC-CLIO. p. 235. ISBN 978-1-57607-345-2.
· "Lycoming PLF1A-2 turbofan engine". Smithsonian National Air and Space Museum. Retrieved December 31, 2021.
· "RB211-535E4" (PDF). Archived from the original (PDF) on 3 January 2011. Retrieved 1 March 2022.
· "p.01.7" (PDF). Icas.rg. Retrieved 1 March 2022.
· Webber, Richard J. (1971). VARIABLE GEOMETRY AFT-FAN FORTAKEOFFQUIETINGOR THRUST AUGMENTATION OF A TURBOJET ENGINE. Ohio: Lewis Research Centre, NASA.
· "The geared turbofan technology – Opportunities, challenges and readiness status" (PDF). Archived from the original (PDF) on 2013-05-20. C. Riegler, C. Bichlmaier:, 1st CEAS European Air and Space Conference, 10–13 September 2007, Berlin, Germany
· Bjorn Fehrm (October 21, 2016). "Bjorn's Corner: The Engine challenge". Leeham News.
· Ben Hargreaves (Sep 28, 2017). "Understanding Complexities Of Bigger Fan Blades". Aviation Week Network.
· Guy Norris and Graham Warwick (Mar 26, 2015). "A Reversed, Tilted Future For Pratt's Geared Turbofan?". Aviation Week & Space Technology.
· Guy Norris (Aug 8, 2017). "Turbofans Are Not Finished Yet". Aviation Week & Space Technology.
· "Continuous Lower Energy, Emissions, and Noise (CLEEN) Program". www.faa.gov. Federal Aviation Administration. Retrieved 11 February 2023.
· Ulrich Wenger (March 20, 2014), Rolls-Royce technology for future aircraft engines (PDF), Rolls-Royce Deutschland
· Dominic Gates (June 15, 2018). "Troublesome advanced engines for Boeing, Airbus jets have disrupted airlines and shaken travelers". The Seattle Times.
· Kerry Reals (6 Sep 2019). "How the future of electric aircraft lies beyond the engines". Flightglobal.
· "Flight Fleet Forecast's engine outlook". Flight Global. 2 November 2016.
· Jane's All the World's Aircraft. 2005. pp. 850–853. ISSN 0075-3017.
· "GEnx". GE.
· "PW1000G". MTU. Archived from the original on 2018-08-18. Retrieved 2016-07-01.
· "The Leap Engine". CFM International.
· The Cambridge Aerospace Dictionary,Bill Gunston 2004,ISBN 978 0 511 33833 5
· Jet Propulsion,Nicholas Cumpsty 1997, ISBN 0 521 59674 2, p.65
· Roth, Bryce; Mavris, Dimitri (2000-07-24). "A comparison of thermodynamic loss models suitable for gas turbine propulsion - Theory and taxonomy". 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Las Vegas,NV,U.S.A.: American Institute of Aeronautics and Astronautics: 4–8. doi:10.2514/6.2000-3714.
· The Cambridge Aerospace Dictionary, Bill Gunston 2004,ISBN 978 0 511 33833 5
· "Reduced Thrust Takeoff". 30 May 2021.
· Gas Turbine Performance Second Edition, Walsh and Fletcher 2004,ISBN 0 632 06434 X, p.5
· Jet Engines and Propulsion Systems For Engineers, Human Resource Development,GE Aircraft Engines 1989,p.5-9
· Aerodynamic Design Of Axial Flow Compressors,N65 23345,1965,NASA SP-36,p.68
· Clancy, L.J., Aerodynamics, page 21
· Introduction To Aerospace Engineering With A Flight Test Perspective,Stephen Corda 2017,ISBN 9781118953389, p.185
3. 外部链接 External links
提示:本部分链接中有些指向无法从中国内地直接访问的站点。
Malcolm Gibson. The Chevron Nozzle: A Novel Approach to Reducing Jet Noise (PDF). NASA Innovation in Aeronautics NASA/TM-2011-216987. Aug 2011 [2020-12-12]. (原始内容存档 (PDF)于2020-03-23).
The Engine Yearbook. UBM Aviation. 2012 [2020-12-12]. (原始内容存档于2020-08-09).
Commercial engines 2017. Flight Global. [2020-12-12]. (原始内容存档于2019-05-26).
Bjorn Fehrm. Bjorn's Corner: Aircraft engines, sum up. Leeham Co. April 14, 2017 [2020-12-12]. (原始内容存档于2021-01-27). and previous series
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