A traction-free-edge hybrid-stress element for the analysis of edge effects in cross-ply laminates
- 1 August 1980
- journal article
- Published by Elsevier in Computers & Structures
- Vol. 12 (2) , 167-179
- https://doi.org/10.1016/0045-7949(80)90002-4
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- A hybrid-stress finite-element formulation for thick multilayer laminatesComputers & Structures, 1980
- Interlaminar Stresses in Symmetric Composite LaminatesJournal of Composite Materials, 1978
- Some New Results on Edge Effect in Symmetric Composite LaminatesJournal of Composite Materials, 1977
- Alternate Hybrid-Stress Elements for Analysis of Multilayer Composite PlatesJournal of Composite Materials, 1977
- Interlaminar Stresses in Composite Laminates—An Approximate Elasticity SolutionJournal of Applied Mechanics, 1974
- On the Calculation of Interlaminar Normal Stress in Composite LaminateJournal of Composite Materials, 1974
- Some observations on the interlaminar strength of composite laminatesInternational Journal of Mechanical Sciences, 1973
- Finite Element Solutions for Laminated Thick PlatesJournal of Composite Materials, 1972
- Approximate Three-Dimensional Solutions for Symmetric Laminates Under Inplane Loading *Journal of Composite Materials, 1971
- Interlaminar Stresses in Composite Laminates Under Uniform Axial ExtensionJournal of Composite Materials, 1970