Volume 31 Issue 02
Feb.  2005
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Jiang Chongwen, Huang Jun, Cao Yihuaet al. Two significant technique requirements in supersonic airliner design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(02): 148-152. (in Chinese)
Citation: Jiang Chongwen, Huang Jun, Cao Yihuaet al. Two significant technique requirements in supersonic airliner design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(02): 148-152. (in Chinese)

Two significant technique requirements in supersonic airliner design

  • Received Date: 20 Jun 2004
  • Publish Date: 28 Feb 2005
  • Supersonic airliner (SSA) is a significant development orientation for the future commercial transport. Two significant technique requirements, based on the study of the payload, range and velocity of new supersonic airliner, was deduced for SSA design. At first, a fuselage arrangement technique applicable to SSA was derived from imitating subsonic airliner fuselage arrangement method in a creative way. The demand of the passenger total to fuselage arrangement was indicated. A sample analysis shows that this technique is reasonable and available in engineering. Secondly, transforming the Breguet range equation with several relative assumptions and using weight estimate gains the relation between the takeoff weight, fuel used in mission and lift-drag radio in cruise. The requirement of SSA operating economics to the lift-drag radio in cruise was obtained. The gained two requirements have significant roles and directional value in multidisciplinary optimization design of SSA.

     

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  • [1] Armstrong S M. High speed research lessons . Report to the NASA Advisory Council, 1999 [2] 索别茨基 H主编.高速运输机设计的新概念[M].钱翼稷 译.北京:国防工业出版社,2001.39,280 Sobieczkyt H. New design concepts for high speed air transport [M]. Translated by Qian Yiji. Beijing:National Defence Industry Press, 2001. 39, 280 (in Chinese) [3] Jenkinson L R, Simpkin P, Rhodes D. Civil jet aircraft design . St Louis:Butterworth-Heinemann, 1999 [4] 中国航空信息中心.世界飞机手册2000[M].北京:航空工业出版社,2001 China Aero Information Center. World aircraft handbook 2000[M]. Beijing:Aviation Industry Press, 2001 (in Chinese) [5] 卢成文主编.世界飞机手册1988[M].北京:航空工业出版社,1988 Lu Chengwen. World’s aircraft handbook 1988 [M]. Beijing:Aviation Industry Press, 1988 (in Chinese) [6] 李为吉主编.现代飞机总体综合设计[M].西安:西北工业大学出版社, 2001 Li Weiji. Modern aircraft concept synthesis design [M]. Xi’an:Northwestern Ploytechnical University Press, 2001 (in Chinese) [7] 杨景佐,曹 名.飞机总体设计[M].北京:航空工业出版社,1991 Yang Jingzuo, Cao Ming. Aircraft concept design [M]. Beijing:Aviation Industry Press, 1991(in Chinese) [8] Raymer D P. Aircraft design:a conceptual approach [M]. Third Edition. Reston, VA:AIAA, 1999 [9] Thivet F, Yan K, Knight D D. Toward the aerodynamical optimization of a supersonic airplane using a genetic algorithm and a PNS solver . 20th AIAA Applied Aerodynamics Conference . St Louis, Missouri, 2002
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