Modelling aeronautical composite laminates behaviour under impact using a saturation damage and delamination continuous material model

Key Engineering Materials

Volumn 452-453, Issue , 2011, Pages 369-372

  Ilyas, Muhammad ^a   Espinosa, Christine ^a   Lachaud, Frédéric ^a   Michel, Laurent ^a   Salaün, Michel ^a  

^a UNIVERSITÉ DE TOULOUSE   (France)

Author keywords

Damage mechanics; Impact; Numerical simulations; Strain rate behavior; Unidirectional composite

Indexed keywords

COMPUTER SIMULATION; STRAIN RATE;

COMPOSITE MATERIAL MODELS; DAMAGE MECHANICS; DYNAMIC CHARACTERIZATION; IMPACT; NUMERICAL PREDICTIONS; RATE BEHAVIOR; UNIDIRECTIONAL COMPOSITES; USER-DEFINED MATERIAL MODEL;

LAMINATED COMPOSITES;

EID: 78650723955     PISSN: 10139826     EISSN: 16629795     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/KEM.452-453.369     Document Type: Conference Paper

References (5)

1. Matzenmiller A., Lubliner R.L., Taylor A., A constitutive model for anisotropic damage in fiber composites, Mechanics of Materials, Vol. 20 (1995), pp 125-152
2. Xiao J.R., Gama, B.A., Gillespie J.W. Jr., Progressive damage and delamination in plain weave S-2 glass/SC-15 composites under quasi-static punch-shear loading, Composites Structures, Vol. 78 (2007), pp 182-196
3. LSTC, LS-DYNA theory manual, ISBN 0-9788540-0-0 (2006)
4. Prombut, P., Caractérisation de la propagation de délaminage des stratifiés composites multidirectionnels. PhD thesis (2007), Université de Toulouse.
5. Ilyas M., Espinosa Ch., Lachaud F., Salaün M., Dynamic delamination using cohesive finite elements, DYMAT 2009