On the Applications of Numerical Methods to Aircraft Running Dynamics

  • Depei Zhu
Conference paper

Abstract

This paper presents some experiences in applications of numerical methods to aircraft running dynamics.

Keywords

Decid 

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References

  1. [1]
    Depei Zhu, Some Dynamic Problems in Design of Aircraft Landing Gear, ICAS-92, Beijing, Sept. (1992), “Proceedings of The 18th Congress of the International Council of the Aeronautical Sciences”, Vol.2, pp. 1341 – 1345.Google Scholar
  2. [2]
    Depei Zhu et al, The Theories and the Preventions of Nose-Wheel Shimmy (in Chinese), Defence Industry Press, Beijing, (1984).Google Scholar
  3. [3]
    Depei Zhu, On Structural Vibration of Aircraft Main Landing Gear, The 2nd Russian-Chinese Symposium on Aircraft Structures, Moscow,Nov. 1992, Proceedings, Vol.2, pp. 6.1 – 6.12, Central Aerohydrodynamics Institute, Zhukovsky, (1992).Google Scholar
  4. [4]
    Depei Zhu, Hui Jin, A Fundamental Model for Dynamic Analysis of a Rolling-up and Spring-back Wheel During Landing Impact (in Chinese), Northwestern Polytechnical University SHJ 8575, (1985).Google Scholar
  5. [5]
    Hui Jin, Jianjun Sun, Depei Zhu, On Dynamic Analysis of a Rolling-up and Spring-back Wheel During Landing Impact (in Chinese), Northwestern Polytechnical University SHJ 8775, (1987).Google Scholar

Copyright information

© Springer-Verlag Berlin Heidelberg 1995

Authors and Affiliations

  • Depei Zhu
    • 1
  1. 1.Northwestern Polytechnical UniversityXianChina

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