Calculation of stiffness matrices for finite elements of thin shellsof arbitrary shape.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 969-972
- https://doi.org/10.2514/3.4653
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- A cylindrical shell discrete element.AIAA Journal, 1967
- 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
- Matrix Displacement Analysis of Anisotropic Shells by Triangular ElementsJournal of the Royal Aeronautical Society, 1965
- Finite Element Solution for Axisymmetrical ShellsJournal of the Engineering Mechanics Division, 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