Ilyas, Muhammad
and Espinosa, Christine and Lachaud, Frédéric and Salaün, Michel
Dynamic delamination modeling using cohesive finite elements.
(2009)
In: 9th International DYMAT Conference on the Mechanical and Physical Behaviour of Materials under Dynamic Loading (DYMAT 2009), 7 September 2009 - 11 September 2009 (Brussels, Belgium).
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(Document in English)
PDF (Author's version ) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 522kB |
Official URL: https://doi.org/10.1051/dymat/2009221
Abstract
In this paper we present a methodology for the prediction of impact induced damage in aeronautical composite structures. Material under consideration is a carbon fiber and epoxy resin (T800S/M21) unidirectional laminate. Continuum damage mechanics is applied for plies and cohesive finite elements are used for delamination prediction. The numerical simulation results from finite element codes are compared with experimental results.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| HAL Id: | hal-02280153 |
| Audience (conference): | International conference proceedings |
| Uncontrolled Keywords: | |
| Institution: | French research institutions > Centre National de la Recherche Scientifique - CNRS (FRANCE) Université de Toulouse > Ecole nationale supérieure des Mines d'Albi-Carmaux - IMT Mines Albi (FRANCE) Université de Toulouse > Institut National des Sciences Appliquées de Toulouse - INSA (FRANCE) Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE) Université de Toulouse > Université Toulouse III - Paul Sabatier - UT3 (FRANCE) |
| Laboratory name: | |
| Statistics: | download |
| Deposited On: | 09 Apr 2009 10:08 |
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