Hostname: page-component-586b7cd67f-dsjbd Total loading time: 0 Render date: 2024-11-24T18:58:33.378Z Has data issue: false hasContentIssue false
  • English
  • Français

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
Get access

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

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

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
5. Fischer, G. Über den Einfluss der gelenkigen Lagerung auf die Stabilität dünnwandiger Kreiszylinderschalen unter Axiallast und Innendruck. Zeitschrift für Flugwissenschaften, Vol. 11, Part 3, p. 111, 1963.Google Scholar