Composite structures;
Delamination failure;
Cohesive zone modelling;
D O I:
10.1007/s10443-012-9257-8
中图分类号:
TB33 [复合材料];
学科分类号:
摘要:
This paper addresses the task of using a commercial non-linear Finite Element code as a design tool to simulate (and design) the behaviour and performance of laminated composite structures. It is shown that the need to model the stress field ahead of a crack tip, in a tiny 'cohesive zone', does not necessarily mean having to use tiny finite elements.
机构:
Technion Israel Inst Technol, Fac Civil & Environm Engn, IL-32000 Haifa, IsraelTechnion Israel Inst Technol, Fac Civil & Environm Engn, IL-32000 Haifa, Israel
机构:
Univ Bordeaux, CNRS, UMR 5801, Lab Composites Thermostruct, 3 Rue La Boetie, F-33600 Pessac, FranceUniv Bordeaux, CNRS, UMR 5801, Lab Composites Thermostruct, 3 Rue La Boetie, F-33600 Pessac, France
Martin, Eric
Vandellos, Thomas
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h-index: 0
机构:
Off Natl Etud & Rech Aerosp, F-92322 Chatillon, France
Herakles Le Haillan, F-33185 Le Haillan, FranceUniv Bordeaux, CNRS, UMR 5801, Lab Composites Thermostruct, 3 Rue La Boetie, F-33600 Pessac, France
Vandellos, Thomas
Leguillon, Dominique
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h-index: 0
机构:
Univ Paris 06, CNRS, UMR 7190, Inst Jean Le Rond dAlembert, 4 Pl Jussieu, F-75005 Paris, FranceUniv Bordeaux, CNRS, UMR 5801, Lab Composites Thermostruct, 3 Rue La Boetie, F-33600 Pessac, France
Leguillon, Dominique
Carrere, Nicolas
论文数: 0引用数: 0
h-index: 0
机构:
Univ Brest, ENSTA Bretagne, LBMS, Brest, FranceUniv Bordeaux, CNRS, UMR 5801, Lab Composites Thermostruct, 3 Rue La Boetie, F-33600 Pessac, France