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On the Applications of Numerical Methods to Aircraft Running Dynamics

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Abstract

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

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References

  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.

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  2. Depei Zhu et al, The Theories and the Preventions of Nose-Wheel Shimmy (in Chinese), Defence Industry Press, Beijing, (1984).

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  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).

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  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).

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  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).

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© 1995 Springer-Verlag Berlin Heidelberg

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Zhu, D. (1995). On the Applications of Numerical Methods to Aircraft Running Dynamics. In: Atluri, S.N., Yagawa, G., Cruse, T. (eds) Computational Mechanics ’95. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-79654-8_437

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  • DOI: https://doi.org/10.1007/978-3-642-79654-8_437

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-79656-2

  • Online ISBN: 978-3-642-79654-8

  • eBook Packages: Springer Book Archive

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