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基于ADAMS/Aircraft的舰载机逃逸性能分析 被引量:2

The Carrier-Based Aircraft Bolter Analysis Based on ADAMS/Aircraft
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摘要 文章基于MSC ADAMS/Aircraft平台,建立了目标舰载机得起落架、轮胎、机身及全机虚拟样机模型,并进行飞机逃逸仿真分析,结果表明目标舰载机具有较好的逃逸性能。 Based on the software ADAMS/Aircraft, the virtual prototype model of the gear, the tire, the airframe and the full aircraft were built in this paper, and the bolter process was simulated. The results show that the aircraft possesses excellent bolter capability, and the ADAMS/Aircraft provides an effective method to the dynamical analysis.
出处 《海军航空工程学院学报》 2010年第5期481-484,共4页 Journal of Naval Aeronautical and Astronautical University
关键词 ADAMS/AIRCRAFT 逃逸 虚拟样机 ADAMS/Aircraft bolter virtual prototype
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参考文献8

  • 1励缨,温玮,金长江.舰载飞机逃逸复飞动力学特性研究[J].飞行力学,1994,12(2):1-9. 被引量:6
  • 2飞机起落架强度设计指南[K].航空航天部科学技术委员会编著,1989.
  • 3ARGERSUBGER W J. The launching and landing of carrier aircraft (Part Four)[R]. AD-21570.
  • 4ETKIN B. Dynamics of Atmospheric Flight[M]. New York: John and Sons, Inc., 1972.
  • 5方振平.飞机飞行动力学[M].北京:北京航空航天大学出版社.2004.
  • 6MDI. Using ADAMS/Aircraft: getting started[K]. 2002.
  • 7MDI. Using ADAMS/Aircraft[K]. Building Templates in ADAMS/Aircraft, 2002.
  • 8MDI. Using ADAM.S/Aircraft[K]. Tire Modeling in ADAMS/Aircraft. 2002.

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