Abstract
Cut ply specimens of IM7/8552 carbon/epoxy laminates were tested under monotonic and cyclic tensile loading. Experimental results were used to validate new cohesive interface element formulations for static and fatigue delamination. Results are presented in terms of static failure loads and fatigue crack growth rates.
| Original language | English |
|---|---|
| Title of host publication | ICCM International Conferences on Composite Materials |
| Publication status | Published - 2009 |
| Event | 17th International Conference on Composite Materials, ICCM-17 - Edinburgh, UK United Kingdom Duration: 27 Jul 2009 → 31 Jul 2009 |
Conference
| Conference | 17th International Conference on Composite Materials, ICCM-17 |
|---|---|
| Country/Territory | UK United Kingdom |
| City | Edinburgh |
| Period | 27/07/09 → 31/07/09 |
Keywords
- Cohesive interface element
- Delamination
- Fatigue
- Ply termination
- Static
ASJC Scopus subject areas
- General Engineering
- Ceramics and Composites
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