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, 07-11 Sept 2009, Brussels, Belgium.
![[img]](http://oatao.univ-toulouse.fr/style/images/fileicons/application_pdf.png) | (Document in English) PDF (Author's version ) - Depositor and staff only - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 510Kb |
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) |
|---|---|
| Audience (conference): | International conference proceedings |
| Uncontrolled Keywords: | |
| Institution: | Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE |
| Laboratory name: | Département de Mécanique des Structures et Matériaux - DMSM (Toulouse, France) - Méthodes Numériques Avancées |
| Statistics: | download |
| Deposited By: | Muhammad ILYAS |
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