The axisymmetric branching behavior of complete spherical shells
Open Access
- 1 January 1981
- journal article
- Published by American Mathematical Society (AMS) in Quarterly of Applied Mathematics
- Vol. 39 (2) , 145-178
- https://doi.org/10.1090/qam/625467
Abstract
The purpose of this paper is to describe the axisymmetric branching behavior of complete spherical shells subjected to external pressure. By means of an asymptotic integration technique (based on the smallness of the ratio of the shell thickness to the shell radius) applied directly to a differential equation formulation, we are able to continue the solution branches from the immediate vicinity of the bifurcation points, where the solution has the functional form predicted by the linear buckling theory, to the region where the solution consists of either one or two “dimples” with the remainder of the shell remaining nearly spherical. The analysis deals with a novel aspect of bifurcation theory involving “closely spaced” eigenvalues.Keywords
This publication has 11 references indexed in Scilit:
- A Course of Modern AnalysisPublished by Cambridge University Press (CUP) ,1996
- Branching from Closely Spaced Eigenvalues with Application to a Model Biochemical ReactionSIAM Journal on Applied Mathematics, 1981
- On large axisymmetrical deflection states of spherical shellsJournal of Elasticity, 1980
- A Collocation Solver for Mixed Order Systems of Boundary Value ProblemsMathematics of Computation, 1979
- Perturbation MethodsIEEE Transactions on Systems, Man, and Cybernetics, 1978
- Spherical Shells Like Hexagons: Cylinders Prefer Diamonds—Part 1Journal of Applied Mechanics, 1973
- The Post-Buckling Problem for Thin Elastic ShellsSIAM Journal on Applied Mathematics, 1971
- Axisymmetric buckling of hollow spheres and hemispheresCommunications on Pure and Applied Mathematics, 1970
- Experimental studies of the postbuckling behavior of complete spherical shellsExperimental Mechanics, 1968
- The Buckling of Spherical Shells by External PressureJournal of the Aeronautical Sciences, 1939