Yoshimura buckling

Yoshimura buckling is a triangular mesh buckling pattern found in thin-walled cylinders under axial compression.[1][2]

This buckling pattern is named after Yoshimaru Yoshimura, the Japanese researcher who first provided an explanation for its development in a paper first published in Japan in 1951,[3] and later republished in the United States in 1955.[4]

References

  1. ↑ de Vries, J., Research on the Yoshimura buckling pattern of small cylindrical thin walled shells, in Proceedings of the European Conference on Spacecraft Structures, Materials and Mechanical Testing 2005 (ESA SP-581). 10–12 May 2005, Noordwijk, The Netherlands. Edited by Karen Fletcher. Bibcode 2005ESASP.581E..21D
  2. ↑ Singer, J.; Arbocz, J.; Weller, T. (2002). Buckling Experiments, Shells, Built-up Structures, Composites and Additional Topics. 2. John Wiley & Sons Ltd. p. 640. ISBN 9780471974505.
  3. ↑ Nicholas J. Hoff (February 1966). "The Perplexing Behavior of Thin Circular Cylindrical Shells in Axial Compression". Stanford University Department of Aeronautics and Astronautics.
  4. ↑ Yoshimaru Yoshimura (July 1955). "On the mechanism of buckling of a circular cylindrical shell under axial compression". National Advisory Committee For Aeronautics.


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