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 |
|---|---|
| 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
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