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On the Linear Buckling of Circular Cylindrical Shells Under Asymmetric Axial Compressive Stress Distributions

Published online by Cambridge University Press:  04 July 2016

D. J. Johns
D. J. Johns*
Affiliation:
Loughborough University of Technology
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Extract

The linear buckling of circular cylindrical shells is considered with particular attention to the cantilever shell subjected to either a pure bending moment (M) or transverse load (P)—see Fig. 1. It is believed that the conclusions reached have wider application to more general loading cases.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 70 , Issue 672 , December 1966 , pp. 1095 - 1097
Copyright
Copyright © Royal Aeronautical Society 1966

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References

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