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The Instability of Buckle Pattern in Cylindrical Shells under Axial Compression

Published online by Cambridge University Press:  07 June 2016

E. H. Mansfield
E. H. Mansfield*
Affiliation:
Royal Aircraft Establishment, Farnborough
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Summary

The repetitive pattern of buckling, common to most theoretical analyses, is shown to be itself unstable. An approximate but very simple analysis is presented to describe the true buckling behaviour.

Type
Research Article
Information
Aeronautical Quarterly , Volume 16 , Issue 3 , August 1965 , pp. 275 - 281
Copyright
Copyright © Royal Aeronautical Society. 1965

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References

1. Thielemann, W. F. New Developments in the Non-Linear Theories of the Buckling of Thin Cylindrical Shells. Aeronautics and Astronautics. Proceedings of the Durand Centenial Conference, p. 76. Edited by Goodier, J. N. and Hoff, N. J.. Pergamon Press, London, 1960.Google Scholar
2. Fung, Y. C. and Sechler, E. E. Instability of Thin Elastic Shells. Proceedings of Symposium on Naval Structural Mechanics, p. 115. Pergamon Press, London, 1960.Google Scholar
3. Kármán, Th. von and Tsien, H. S. The Buckling of Thin Cylindrical Shells under Axial Compression. Journal of the Aeronautical Sciences, Vol. 8, No. 8, p. 303, 1941.CrossRefGoogle Scholar
4. Nachbar, W. and Hoff, N. J. The Buckling of a Free Edge of an Axially-Compressed Circular Cylindrical Shell. Quarterly of Applied Mathematics, Vol. 20, No. 3, p. 267, 1962.Google Scholar
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