The Elastic Instability of a Complete Spherical Shell
- 1 May 1962
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 13 (2), 189-201
- https://doi.org/10.1017/s0001925900002377
Abstract
Summary The elastic instability of a complete spherical shell under uniform external pressure is studied experimentally and theoretically. The premature snapping of a thin elastic shell, made of polyvinyl chloride, is seen to be classical in nature. The experimental maximum pressure and pre-snapping bending deformation are correlated with the theoretical behaviour of an initially imperfect shell. The large deflection behaviour of a perfect shell is assessed experimentally, and the stable post-buckling states are observed to be rotationally symmetric. A fairly precise theoretical analysis of these states is performed, the use of a high-speed digital computer allowing a considerable advance over previous treatments. The experimental and theoretical post-buckling curves are in good agreement, yielding the first detailed correlation of post-snapping equilibrium states in the field of shell instability.Keywords
This publication has 4 references indexed in Scilit:
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- Postbuckling Behavior of Axially Compressed Circular Cylindrical ShellsJournal of the Aeronautical Sciences, 1954
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950
- A Theory for the Buckling of Thin ShellsJournal of the Aeronautical Sciences, 1942