Direct stiffness method analysis of shells of revolution utilizing curved elements.
- 1 September 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (9), 1519-1525
- https://doi.org/10.2514/3.3729
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- 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
- Finite Element Solution for Axisymmetrical ShellsJournal of the Engineering Mechanics Division, 1964
- A generalization of the direct-stiffness method of structural analysisAIAA Journal, 1964
- ANALYSIS OF AXISYMMETRICAL SHELLS BY THE DIRECT STIFFNESS METHODAIAA Journal, 1963
- CONICAL SEGMENT METHOD FOR ANALYZING OPEN CROWN SHELLS OF REVOLUTION FOR EDGE LOADINGAIAA Journal, 1963