On the Linear Buckling of Circular Cylindrical Shells Under Asymmetric Axial Compressive Stress Distributions
- 4 July 1966
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of the Royal Aeronautical Society
- Vol. 70 (672) , 1095-1097
- https://doi.org/10.1017/s0368393100083243
Abstract
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.Keywords
This publication has 3 references indexed in Scilit:
- Buckling of cantilever cylindrical shell with a transverse end load.AIAA Journal, 1965
- On the Buckling of Circular Cylindrical Shells Under Pure BendingJournal of Applied Mechanics, 1961
- Thermal Buckling of Circular Cylindrical Shells Under Circumferential Temperature GradientsJournal of the Aerospace Sciences, 1959