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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
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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

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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