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Volume 28 Issue 5
May  2002
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Journal of Beijing University of Aeronautics and Astronautics  > 2002  >  28(5): 570-573.
Chen Lei, Chen Zongji. Vision-based autonomous landing integrated navigation scheme of unmanned combat aerial vehicles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(02): 159-163. (in Chinese)
Citation: LIU Xiao-dong, LIU Wen-ting, WANG Zhenget al. Loading Spectra Development for Special Structural Members of Fighter[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(5): 570-573. (in Chinese)
shu

Loading Spectra Development for Special Structural Members of Fighter

  • 1.

    Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • 2. Chengdu Aircraft Design and Research Institute

  • Received Date: 26 Feb 2001
  • Publish Date: 31 May 2002
    Abstract
  • The approach and specialties of loading spectra development using maneuvers simulation technique for new-design aircraft were introduced in brief. Onthe above basis, the approach and key-points of developing stress/pressure spectrum for integral tank, gusts and sideslip spectrum for vertical tail were presented in detail. One key step of developing stress/pressure spectrum for integral tank is to calculate the pressure of the tank in all loading cases, and the G-A-G cycle should be taken into account for the analysis spectrum of the tank. The loading spectrum of the vertical tail is obtained by not only the simulation of maneuvers but also some statistical measurements.

     

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    • References(1)
  • [1] Hewitt R L, Hiscockss R J, Bernard G. Loading spectrum determination for an aircraft with a digital flight control system—CF18 centre fuselage example[J]. Canadian Aeronautics and Space Journal, 1996,42(1):5~9. [2]王世伟.军用飞机疲劳·损伤容限·耐久性设计手册总论[M]. 北京:中国航空研究院, 1994. 17~55.
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