Publication :


Title:

Dynamic delamination of aeronautic structural composites by using cohesive finite elements

Authors: M. Ilyas, F. Lachaud, C. Espinosa and M. Salaün
Year: juillet 2009
Proceedings de : 17th International Conference on Composite Materials (ICCM-17), 27-31 July 2009, Edinburgh (GB).

OATAO: 3537

Abstract:
Cohesive finite elements are used to model impact induced delamination prediction of T800/21M unidirectional laminated composite. DCB, ELS and MMB tests are used to identify cohesive element parameters. Results from experiments and numerical prediction of impact induced delamination by commercially available code LS-DYNA are compared.

Bibtex citation :
@INPROCEEDINGS{Ilyas2009,
Author={Ilyas, M. and Lachaud, F. and Espinosa, C. and Sala\"un, M.},
Title={Dynamic delamination of aeronautic structural composites by using cohesive finite elements},
Booktitle={17th International Conference on Composite Materials (ICCM-17), 27-31 July 2009, Edinburgh (GB)},
Pages={},
Year={2009}}


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