Nonlinear analysis of shells of revolution by the matrix displacement method.
- 1 December 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (12), 2306-2312
- https://doi.org/10.2514/3.4987
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Rigid-body displacements of curved elements in the analysis of shells by the matrix- displacement method.AIAA Journal, 1967
- ANALYSIS OF ELASTIC STABILITY OF SHELLS OF REVOLUTION BY THE FINITE ELEMENT METHOD?Published by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Improvements on the analysis of shells of revolution by the matrix displacement method.AIAA Journal, 1966
- Direct stiffness method analysis of shells of revolution utilizing curved elements.AIAA Journal, 1966
- Computation of stress resultants from the element stiffness matrices.AIAA Journal, 1966
- Application of matrix displacement method to linear elastic analysisof shells of revolution.AIAA Journal, 1965
- 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