前翼（鸭翼）/ Canard (aeronautics) – 中英文维基百科词条融合

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1. 正文（发布于知乎专栏）

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2. 参见（维基百科的相关词条）| See also

3. 参考文献 | References

3.1 英文词条引用列表 | Citations

  1. ^ Wragg, D.; Historical Dictionary of Aviation, History Press (2008), Page 79.
  2. ^ Jump up to:a b Clancy, L. J. (1975). Aerodynamics, Pitman (UK), Halsted (US), 1975. Pages 292-3.
  3. ^ Crane, Dale (1997), Dictionary of Aeronautical Terms (3rd ed.), Aviation Supplies & Academics, p. 86, ISBN 978-1-56027-287-8.
  4. ^ Aerodynamic analysis of a canard missile configuration using ANSYS Calhoun: The NPS Institutional Archive, December 2011. Retrieved 16 June 2021
  5. ^ Effect of Tail-Fin Span on Stability and Control Characteristics of a Canard-Controlled Missile at Supersonic Mach Numbers NASA Technical paper 2157, June 1983. Retrieved 16 June 2021
  6. ^ Laser Guided Bombs FAS Military Analysis Network, 12 February 2000. Retrieved 16 June 2021
  7. ^ Villard, Henry Serrano (2002). Contact! : the story of the early aviators. Mineola, NY: Dover Publications. pp. 39–53. ISBN 978-0-486-42327-2.
  8. ^ Burns 1983.
  9. ^ Kundu, Ajoy Kumar; Price, Mark A.; Riordan, David (8 April 2019). Conceptual Aircraft Design: An Industrial Approach. John Wiley and Sons. p. 237.
  10. ^ Culick, F.E.C. (2003). “The Wright Brothers: First Aeronautical Engineers and Test Pilots” (PDF). AIAA Journal. 41 (6): 985–1006. Bibcode:2003AIAAJ..41..985C. CiteSeerX 10.1.1.579.7665. doi:10.2514/2.2046. Retrieved 8 August 2015.
  11. ^ Jerram, Michael E. Incredible Flying Machines. Marshall Cavendish, 1980. p.59.
  12. ^ Flight, Flight global, 14 March 1914, p. 286.
  13. ^ Green, W; Swanborough, G (1994), The complete book of fighters, Salamander, p. 163.
  14. ^ Jump up to:a b c Delta wing canard aircraft, US Patent US3188022 A.
  15. ^ Anderson, S.B.; A Look at Handling Qualities of Canard Configurations, NASA Technical Memorimdum 88354, 1986, page 21.
  16. ^ Jump up to:a b Stinton, Daroll, The design of the aeroplane, Rutan canards wrought a change in thinking which might have a profound influence in future.
  17. ^ Anderson, Seth B. (September 1986). “A look at Handling Qualities of Canard Configurations” (PDF). NASA Technical Memorandum 88354: 4–5.
  18. ^ Pocock, Chris (15 November 2013). “Swiss Battle Could Be Euro-Canard Turning Point”. Aviation International News.
  19. ^ “JAST hover tests to start in June”. Flight Global.
  20. ^ “Future Fighter Investment Is Keeping Eurocanards Competitive | Aviation Week Network”. aviationweek.com.
  21. ^ Jump up to:a b Drela, Mark, Aero-astro professor, MIT, Canard description (forum), RC universe, archived from the original on 30 June 2013.
  22. ^ Jump up to:a b c Neblett, Metheny & Leifsson 2003.
  23. ^ Jump up to:a b A Summary of Canard Advantages and Disadvantages, Desktop Aero, archived from the original on 3 May 2015, retrieved 6 October 2015.
  24. ^ Jump up to:a b c d Raymer, Daniel P. (1999). Aircraft Design: A Conceptual Approach (3 ed.). AIAA. ISBN 978-1-56347-281-7.
  25. ^ Gudmondsson, Snorri (3 September 2013). General Aviation Aircraft Design: Applied Methods and Procedures. Elsevier Inc.
  26. ^ Garrison (2002), page 85; “the stabilizer in the front… This is the function of the stabilizer. If it’s in the back it typically pushes downward, and if it’s in the front it lifts upward.”
  27. ^ Benson, T (ed.), “Airplane parts and functions”, Beginner’s Guide to Aeronautics, NASA Glenn Research Center, archived from the original on 31 May 2022, retrieved 30 July 2013, On the Wright brother’s first aircraft, the horizontal stabilizer was placed in front of the wings.
  28. ^ Aircraft with reduced wing structure loading (patent), US, 6064923 A, …a front stabilizer, generally known as a canard stabilizer…
  29. ^ X-29 (fact sheet), Dryden: Nasa, 9 September 2015, FS-008-DFRC, The X-29… while its canards—horizontal stabilizers to control pitch—were in front of the wings instead of on the tail.
  30. ^ Culick, AIAA-2001-3385, Consistently with ignoring the condition of zero net (pitch) moment, the Wrights assumed that in equilibrium the canard carried no load and served only as a control device.
  31. ^ Anderson, Seth B (1987). “A look at handling qualities of canard configurations”. Journal of Guidance, Control, and Dynamics. 10 (2): 8. Bibcode:1987JGCD…10..129A. doi:10.2514/3.20194. hdl:2060/19870013196. TM 88354. …the Flyer was highly unstable… The lateral/directional stability and control of the Flyer were marginal.
  32. ^ Garrison (2002), page 85; “Because the center of gravity is not sitting right on top of the center of lift, but is ahead of it, the aircraft would tip over forard if some balancing force were not provided. This is the function of the stabilizer.”
  33. ^ Jump up to:a b Sherwin, Keith (1975). Man powered flight (rev reprint ed.). Model & Allied Publications. p. 131. ISBN 978-0-85242-436-0..
  34. ^ Hoerner, “Aspect ratio”, Fluid Dynamic Lift, pp. 11–30.
  35. ^ “Lift-induced drag”, Wikipedia, 25 September 2019, retrieved 17 March 2020
  36. ^ Jump up to:a b VariEze Wind Tunnel Investigation, Nasa, TP 2382.
  37. ^ Tandem aircraft PAT-1, Nasa, TM 88354.
  38. ^ Anderson, Seth B (1 September 1986), “A Look at Handling Qualities of Canard Configurations” (PDF), Journal of Guidance, Control, and Dynamics, 10 (2): 16, Bibcode:1987JGCD…10..129A, doi:10.2514/3.20194, hdl:2060/19870013196, TM-88354, Incorporating roll control on the canard is basically less efficient because of an adverse downwash influence on the main wing opposing the canard rolling-moment input.
  39. ^ “Jet Aircraft – Effect of a close-coupled canard on a swept wing”. SAI Research Report (Abstract). Sage Action. 2009. 7501. Archived from the original on 19 February 2015. Retrieved 25 August 2009.
  40. ^ NASA Conference Publication, Issues 2-3. Scientific and Technical Information Office, National Aeronautics and Space Administration. 1977. pp. 1–2.
  41. ^ Probert, B, Aspects of Wing Design for Transonic and Supersonic Combat, NATO, archived from the original (PDF) on 17 May 2011.
  42. ^ Aerodynamic highlights of a fourth generation delta canard fighter aircraft, Mach flyg, archived from the original on 27 November 2014.
  43. ^ Jones, Lloyd S.; U.S. Fighters: Army – Air Force 1925 to 1980s, Aero, pp.139-41.
  44. ^ Roskam, J (1989), Airplane Design: Preliminary Configuration Design and Integration of the Propulsion System, Design Analysis & Research, p. 82, ISBN 978-1-884885-43-3.
  45. ^ Group, Techbriefs Media. “Conformably Stowable Canard”. www.techbriefs.com. Retrieved 17 March 2020.
  46. ^ Conformably Stowable Canard (tech brief), Ames Research Center, archived from the original on 15 September 2012.
  47. ^ Jones (1974), “US Bombers”, Aero, canard vanes.
  48. ^ “B-1 Roll-out”, Flight, 1974, canard fins for ride control.
  49. ^ Sweetman, William ‘Bill’ (June 1997), “Top Gun”, Popular Science: 104.
  50. ^ “FAQ Eurofighter (translation).” Retrieved 29 November 2009.
  51. ^ “Austrian Eurofighter committee of inquiry: Brigadier Dipl.Ing.Knoll about Eurofighter and Stealth, pp. 76–77. (English translation)” Google. Retrieved 28 November 2009.
  52. ^ Sweetman, William ‘Bill’ (14 January 2011), “From JAST To J-20”, Aviation Week.
  53. ^ Sweetman, William ‘Bill’ (2005). Lockheed Stealth. Zenith Press. pp. 122–24 [124]. ISBN 978-0-7603-1940-6.[permanent dead link]
  54. ^ “Agility+Stealth = X-36: formula for an advanced fighter “ Archived 2014-02-23 at the Wayback Machine Design News 14 January 2013
  55. ^ Roblin, Sebastien (9 November 2021). “How Stealthy is China’s J-20 Fighter Jet?”. The National Interest.
  56. ^ “Stealth”. chengdu-j-20.
  57. ^ “Chengdu J-20 Overhyped or Reality – A Comprehensive Story”. 15 August 2020.
  58. ^ Suciu, Peter. “Why China’s and Russia’s 5th-generation stealth jets don’t quite live up to the hype, according to a former US Navy pilot”. Business Insider.

3.2 英文词条来源文献 | Bibliography

3.3 中文词条

  1. ^ 跳转到：1.0 1.1 Jonh Anderson. Introduce to Flight，5th. ed.. New York: McGRAW-Hill. 2005. ISBN 0071238182.
  2. ^ Warren Phillips. Mechanics of Flight. Hoboken: Wiley. 2004. ISBN 0471334588.

4. 延伸阅读 | Further reading

  • Abzug; Larrabee (2002), Airplane Stability and Control, Cambridge University Press, ISBN 9781107321427, OCLC 829704722.
  • Gambu, J; Perard, J (January 1973), “Saab 37 Viggen”, Aviation International, no. 602, pp. 29–40.
  • Lennon, Andy (1984), Canard : a revolution in flight, Aviation.
  • Rollo, Vera Foster (1991), Burt Rutan Reinventing the Airplane, Maryland Historical Press.
  • Wilkinson, R (2001). Aircraft Structures and Systems (2nd ed.). MechAero Publishing.
  • Selberg, Bruce P; Cronin, Donald L, Aerodynamic-Structural Study of Canard Wing, Dual Wing, and Conventional Wing Systems for General Aviation Applications. University of Missouri-Rolla. Contract Report 172529, National Aeronautics and Space Administration Aerodynamic-structural study of canard wing, dual wing, and conventional wing systems for general aviation applications

5. 外部链接 | External links

Wikimedia Commons has media related to Canard wings.【维基共享资源中拥有与鸭翼相关的媒体。】

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