Abstract
The elastic solution in the vicinity of a traction free edge and an interface crack in cross-ply anisotropic laminates is provided in details for three problems. Complex eigen-pairs and edge stress intensity functions are computed with high accuracy, aimed to serve as benchmark problems against which other numerical methods can be checked.
Original language | English |
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Pages (from-to) | 1216-1224 |
Number of pages | 9 |
Journal | Composites Science and Technology |
Volume | 68 |
Issue number | 5 |
DOIs | |
State | Published - 1 Apr 2008 |
Keywords
- A. Laminate
- B. Delamination
- C. Finite-element analysis (FEA), Crack
- Edge stress intensity factors
ASJC Scopus subject areas
- Ceramics and Composites
- General Engineering