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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*
Affiliation:
Loughborough University of Technology

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
Copyright
Copyright © Royal Aeronautical Society 1966

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References

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