Strain-energy-release rate analysis of delamination around an open hole in composite laminates
- 14 May 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- DETERMINATION OF INTERLAMINAR FRACTURE TOUGHNESS AND FRACTURE MODE DEPENDENCE OF COMPOSITES USING THE EDGE DELAMINATION TESTPublished by Elsevier ,1983
- Three-Dimensional Analysis of [0/90]s and [90/0]s Laminates with a Central Circular HoleJournal of Composites Technology and Research, 1982
- Interlaminar stress singularities at a straight free edge in composite laminatesComputers & Structures, 1981
- An Energy Release Rate Approach For Stable Crack Growth in the Free-Edge Delamination ProblemJournal of Composite Materials, 1977
- Some observations on the interlaminar strength of composite laminatesInternational Journal of Mechanical Sciences, 1973