ANALYSIS OF ELASTIC STABILITY OF SHELLS OF REVOLUTION BY THE FINITE ELEMENT METHOD?
- 29 March 1967
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- A discrete element procedure for thin-shell instability analysis.AIAA Journal, 1967
- Improvements on the analysis of shells of revolution by the matrix displacement method.AIAA Journal, 1966
- Application of matrix displacement method to linear elastic analysisof shells of revolution.AIAA Journal, 1965
- Consistent matrix formulations for structural analysis using finite-element techniques.AIAA Journal, 1965
- Buckling of circular cylindrical shells in axial compressionInternational Journal of Mechanical Sciences, 1965
- BUCKLING OF A TRUNCATED HEMISPHERE UNDER AXIAL TENSIONAIAA Journal, 1963
- Nonlinear theories for thin shellsQuarterly of Applied Mathematics, 1963
- On the Buckling of Truncated Conical Shells in TorsionJournal of Applied Mechanics, 1962
- Intermittent Release of Smoke from ChimneysJournal of Mechanical Engineering Science, 1960
- Large Deflections of Structures Subjected to Heating and External LoadsJournal of the Aerospace Sciences, 1960