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Aero-Hydroelasticity and Stress of Spacers for Fuel Elements as Structural Anisotropic Domes Composed of Cylindrical Shells

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Computational Mechanics ’86

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Summary

The results of investigations concerning the stability limit and the state of stress in the spacers which are assumed to be the structural anisotropic domes composed of cylindrical shells are presented. The developed cascade method of free parameters suitable for the numerical solution of the problem with the help of a computer is described. An application from the region of the spacers for nuclear reactors - including the numerical results and correlation with the case of the plate - type spacers - is shown.

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References

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Author information

Authors and Affiliations

  1. Reactor Mechanics Group, National Research Institute for Machine Design, 250 97, Prague 9, Czechoslovakia

    V. Kuželka

Authors
  1. V. Kuželka
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Editor information

Editors and Affiliations

  1. Department of Nuclear Engineering, The University of Tokyo, 3-1, Hongo 7-chome, Bunkyo-ku, Tokyo 113, Japan

    Genki Yagawa

  2. Center for the Advancement of Computational Mechanics, School of Civil Engineering, Georgia Institute of Technology, 225, North Avenue, Atlanta, GA, 30332, USA

    Satya N. Atluri

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© 1986 Springer Japan

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Kuželka, V. (1986). Aero-Hydroelasticity and Stress of Spacers for Fuel Elements as Structural Anisotropic Domes Composed of Cylindrical Shells. In: Yagawa, G., Atluri, S.N. (eds) Computational Mechanics ’86. Springer, Tokyo. https://doi.org/10.1007/978-4-431-68042-0_38

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  • DOI: https://doi.org/10.1007/978-4-431-68042-0_38

  • Publisher Name: Springer, Tokyo

  • Print ISBN: 978-4-431-68044-4

  • Online ISBN: 978-4-431-68042-0

  • eBook Packages: Springer Book Archive

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