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。

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。

: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。

  1. · Marshall Brain (April 2000). "How Gas Turbine Engines Work". howstuffworks.com. Retrieved 2010-11-24.

  2. · 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.

  3. · 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 [...]

  4. · 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…

  5. · 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.

  6. · Thrust Augmentation with Mixer/Ejector systems,Presz,Reynolds,Hunter,AIAA 2002-0230,p.3

  7. · Gas Turbine Aerothermodynamics With Special Reference To Aircraft propulsion,Sir Frank Whittle 1981,ISBN 0 08 026719 X, p.217

  8. · Gas Turbine Aerothermodynamics With Special Reference To Aircraft propulsion,Sir Frank Whittle 1981,ISBN 0 08 026719 X, p.218

  9. · 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.

  10. · Roth, Bryce Alexander (2000-09-01). A theoretical treatment of technical risk in modern propulsion system design (Thesis). Bibcode:2000PhDT.......101R. p.76

  11. · Journal of Aircraft September-October 1966: Vol 3 Iss 5. Internet Archive. American Institute of Aeronautics and Astronautics. September 1966. p. 386.

  12. · Journal of Aircraft September-October 1966: Vol 3 Iss 5. Internet Archive. American Institute of Aeronautics and Astronautics. September 1966. p. 387.

  13. · "Bypass ratio", Britannica

  14. · Thermodynamics, MIT, archived from the original on 2013-05-28

  15. · 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

  16. · "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

  17. · "Flight global" (PDF). Flightglobal.com.

  18. · Taylor, John W.R. (ed.), All The World's Aircraft 1975–1976, Paulton House, 8 Sheperdess Walk, London N1 7LW: Jane's, p. 748

  19. · Proceedings, ASME, 15 April 2015, doi:10.1115/84-GT-230

  20. · "PW tales", Road runners Internationale

  21. · "Turbofan Engine". GRC NASA. Retrieved 2010-11-24.

  22. · 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.

  23. · "The turbofan engine" Archived 2015-04-18 at the Wayback Machine, p. 7. SRM Institute of Science and Technology, Department of Aerospace Engineering.

  24. · Cohen; Rogers; Saravanamuttoo (1972). Gas Turbine Theory (2nd ed.). Longmans. p. 85. ISBN 0-582-44927-8.

  25. · FAA-H-8083-3B Airplane Flying Handbook Handbook (PDF). Federal Aviation Administration. 2004. Archived from the original (PDF) on 2012-09-21.

  26. · "Turbofan Thrust". Grc.nasa.gov. Retrieved 1 March 2022.

  27. · 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.

  28. · Kempton, A., "Acoustic liners for modern aero-engines", 15th CEAS-ASC Workshop and 1st Scientific Workshop of X-Noise EV, 2011. Win.tue.nl.

  29. · Smith, Michael J. T. (19 February 1970). "Softly, softly towards the quiet jet". New Scientist. fig. 5.

  30. · 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.

  31. · Smith, M.J.T. (17 August 1972). "Quiet Propulsion". Flight International. p. 241.

  32. · McAlpine, A., Research project: Buzz-saw noise and nonlinear acoustics, University of Southampton

  33. · 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

  34. · 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

  35. · Banke, Jim (2012-12-13). "NASA Helps Create a More Silent Night". NASA. Retrieved January 12, 2013.

  36. · 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.

  37. · "Invited" (PDF), 13th ACFM, CN: AFMC, archived from the original (PDF) on 2014-03-25

  38. · "Turbojet History And Development 1930–1960 Volume 1", The Crowood Press Ltd. 2007, ISBN 978 1 86126 912 6, p. 241.

  39. · "Metrovick F3 Cutaway – Pictures & Photos on FlightGlobal Airspace". Flightglobal.com. 2007-11-07. Retrieved 2013-04-29.

  40. · "page 145". Flight international. 1946.

  41. · "1954 | 0985 | Flight Archive". Flightglobal.com. 1954-04-09. Retrieved 2013-04-29.

  42. · The Development Of Jet And Turbine Aero Engines 4th edition, Bill Gunston 2006, ISBN 0 7509 4477 3, p. 197.

  43. · Boyne, Walter J., ed. (2002). Air warfare: An international encyclopedia: A–L. ABC-CLIO. p. 235. ISBN 978-1-57607-345-2.

  44. · "Lycoming PLF1A-2 turbofan engine". Smithsonian National Air and Space Museum. Retrieved December 31, 2021.

  45. · "RB211-535E4" (PDF). Archived from the original (PDF) on 3 January 2011. Retrieved 1 March 2022.

  46. · "p.01.7" (PDF). Icas.rg. Retrieved 1 March 2022.

  47. · Webber, Richard J. (1971). VARIABLE GEOMETRY AFT-FAN FORTAKEOFFQUIETINGOR THRUST AUGMENTATION OF A TURBOJET ENGINE. Ohio: Lewis Research Centre, NASA.

  48. · "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

  49. · Bjorn Fehrm (October 21, 2016). "Bjorn's Corner: The Engine challenge". Leeham News.

  50. · Ben Hargreaves (Sep 28, 2017). "Understanding Complexities Of Bigger Fan Blades". Aviation Week Network.

  51. · Guy Norris and Graham Warwick (Mar 26, 2015). "A Reversed, Tilted Future For Pratt's Geared Turbofan?". Aviation Week & Space Technology.

  52. · Guy Norris (Aug 8, 2017). "Turbofans Are Not Finished Yet". Aviation Week & Space Technology.

  53. · "Continuous Lower Energy, Emissions, and Noise (CLEEN) Program". www.faa.gov. Federal Aviation Administration. Retrieved 11 February 2023.

  54. · Ulrich Wenger (March 20, 2014), Rolls-Royce technology for future aircraft engines (PDF), Rolls-Royce Deutschland

  55. · Dominic Gates (June 15, 2018). "Troublesome advanced engines for Boeing, Airbus jets have disrupted airlines and shaken travelers". The Seattle Times.

  56. · Kerry Reals (6 Sep 2019). "How the future of electric aircraft lies beyond the engines". Flightglobal.

  57. · "Flight Fleet Forecast's engine outlook". Flight Global. 2 November 2016.

  58. · Jane's All the World's Aircraft. 2005. pp. 850–853. ISSN 0075-3017.

  59. · "GEnx". GE.

  60. · "PW1000G". MTU. Archived from the original on 2018-08-18. Retrieved 2016-07-01.

  61. · "The Leap Engine". CFM International.

  62. · The Cambridge Aerospace Dictionary,Bill Gunston 2004,ISBN 978 0 511 33833 5

  63. · Jet Propulsion,Nicholas Cumpsty 1997, ISBN 0 521 59674 2, p.65

  64. · 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.

  65. · The Cambridge Aerospace Dictionary, Bill Gunston 2004,ISBN 978 0 511 33833 5

  66. · "Reduced Thrust Takeoff". 30 May 2021.

  67. · Gas Turbine Performance Second Edition, Walsh and Fletcher 2004,ISBN 0 632 06434 X, p.5

  68. · Jet Engines and Propulsion Systems For Engineers, Human Resource Development,GE Aircraft Engines 1989,p.5-9

  69. · Aerodynamic Design Of Axial Flow Compressors,N65 23345,1965,NASA SP-36,p.68

  70. · Clancy, L.J., Aerodynamics, page 21

  71. · 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。