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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2003, Vol. 24 ›› Issue (6): 517-520.

• 论文 • Previous Articles     Next Articles

Parameters Study at Touchdown Instant of the Nose Undercarriage of Fighter Airplane

SHI Hai-wen1, YANG Shu-xun2, ZHANG Da-qian3, FU Yong-hong4   

  1. 1. Institute of Solid Mechanics; Beijing University of Aeronautics and Astronuntics; Beijing 100083; China;2. Shenyang Aircraft Design & Research Institute; Shenyang 110035; China;3. Shenyang Institute of Aeronautics Engineering; Shenyang 110031; China;4. Shenyang Aircraft Corporation; Shenyang 110034; China
  • Received:2002-09-11 Revised:2002-11-05 Online:2003-12-25 Published:2003-12-25

Abstract: The status of an under carr iag e at t he touchdow n instant is studied by analyzing the undercar riage par ameters w hich chang e w ith the w heel rotational speed in the drop test. The result indicates that when the spin-up horizo ntal load is the max imum dur ing t he landing , the opposite course residual elasticity of the under carriag e is not finished, and when the opposite course residual elasticity of t he under carr iag e is the max imum, the w heel mov ement ischanged from slide to roll.

Key words: undercarriage, drop test, wheel, rotational speed, horizontal load

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