Hostname: page-component-cd9895bd7-gvvz8 Total loading time: 0 Render date: 2024-12-22T15:28:47.146Z Has data issue: false hasContentIssue false
  • English
  • Français

Interaction Between Membrane and Edge Stresses for Thin Cylinders Under Axially Symmetrical Loading

Published online by Cambridge University Press:  04 July 2016

W. H. Wittrick
W. H. Wittrick*
Affiliation:
Department of Aeronautical Engineering, University of Sydney
Get access Rights & Permissions [Opens in a new window]

Summary

The effect of the longitudinal membrane stress on the flexural edge stresses in a thin cylinder under axially symmetrical loading is considered. A general solution is given, and applied to two specific problems to illustrate the magnitude of the effect.

Type
Research Article
Information
The Aeronautical Journal , Volume 67 , Issue 627 , March 1963 , pp. 172 - 174
Copyright
Copyright © Royal Aeronautical Society 1963

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.Timoshenko, S. (1936). Theory of Elastic Stability. McGraw– Hill. First Edition, 1936.Google Scholar
2.Timoshenko, S. (1940). Theory of Plates and Shells. McGraw–Hill. First Edition, 1940.Google Scholar
3.Menkes, E. G. (1962). A Note on Discontinuity Stresses in Cylindrical Shells. Journal of the Aerospace Sciences, Vol. 29, p. 619, May 1962.Google Scholar