Abstract
In this paper a hierarchical FE approach is utilized to simulate delamination in a composite plate
loaded in uni-axial compression. Progressive delamination is modelled by use of cohesive interface
elements that are automatically embedded. The non-linear problem is solved quasi-statically in which
the interaction between material degradation and structural instability is solved iteratively. The effect
of fibre bridging is studied numerically and in-plane failure is predicted using physically based failure
criteria.
loaded in uni-axial compression. Progressive delamination is modelled by use of cohesive interface
elements that are automatically embedded. The non-linear problem is solved quasi-statically in which
the interaction between material degradation and structural instability is solved iteratively. The effect
of fibre bridging is studied numerically and in-plane failure is predicted using physically based failure
criteria.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of Composites 2009 |
| Number of pages | 6 |
| Publication date | 2009 |
| Publication status | Published - 2009 |
| Event | 2nd ECCOMAS Thematic Conference on the Mechanical Response of Composites - London, United Kingdom Duration: 1 Apr 2009 → 3 Apr 2009 |
Conference
| Conference | 2nd ECCOMAS Thematic Conference on the Mechanical Response of Composites |
|---|---|
| Country/Territory | United Kingdom |
| City | London |
| Period | 01/04/2009 → 03/04/2009 |