XFEM simulation of delamination in composite laminates. (January 2016)

• Record Type: Journal Article
• Authors: Zhao, Libin; Zhi, Jie; Zhang, Jianyu; Liu, Zhanli; Hu, Ning
• Is Part Of: Composites. Volume 80(2016)
• Page Start: 61
• Page End: 71
• Publication Date: 2016-01
• Subjects: B. Delamination -- B. Fracture -- C. Computational modeling -- C. Finite element analysis (FEA); Composite materials -- Periodicals; Manufacturing processes -- Periodicals; Composite materials; Manufacturing processes; Periodicals; 620.11805
• DOI: 10.1016/j.compositesa.2015.10.007
• Languages: English
• ISSNs: 1359-835X

Abstract

Abstract: In this paper, the extended finite element method (XFEM) is extended to simulate delamination problems in composite laminates. A crack-leading model is proposed and implemented in the ABAQUS® to discriminate different delamination morphologies, i.e., the 0°/0° interface in unidirectional laminates and the 0°/90° interface in multidirectional laminates, which accounts for both interlaminar and intralaminar crack propagation. Three typical delamination problems were simulated and verified. The results of single delamination in unidirectional laminates under pure mode I, mode II, and mixed mode I/II correspond well with the analytical solutions. The results of multiple delaminations in unidirectional laminates are in good agreement with experimental data. Finally, using a recently proposed test that characterizes the interaction of delamination and matrix cracks in cross-ply laminates, the present numerical results of the delamination migration caused by the coupled failure mechanisms are consistent with experimental observations.