纤维增强复合材料层合板分层扩展行为研究进展

doi:10.7527/S1000-6893.2018.22509

Abstract

Abstract: Fiber reinforced composites are widely used in aerospace and other engineering fields. Delamination is the main damage form in fiber reinforced composite laminates and also has been one of the focuses of composite mechanics. In this paper, the research achievements about the delamination in fiber reinforced composites at home and abroad are systematically surveyed from three aspects:the experimental research, mechanical model, and numerical simulation. The fracture toughness test methods and theories for modes I, Ⅱ, and mixed I/Ⅱ delamination of unidirectional composites and experimental researches on delamination of multidirectional composites are introduced. The fiber bridging model, the delamination growth criterion, and the fatigue delamination model for characterizing and evaluating the delamination behavior are concluded. In addition, the research status of the numerical simulation on delamination carried out by the Cohesive Zone Model (CZM), the Virtual Crack Closure Technique (VCCT) and the Extended Finite Element Method (XFEM) are expatiated. Finally, the future development directions of delamination in composite materials are prospected.

Key words: reinforced composite, laminate, delamination, fracture toughness, fatigue delamination growth rate

CLC Number:

V214.8

ZHAO Libin, GONG Yu, ZHANG Jianyu. A survey on delamination growth behavior in fiber reinforced composite laminates[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(1): 522509-522509.

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A survey on delamination growth behavior in fiber reinforced composite laminates

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