Displacement Rate Effects on the Mode II Shear Delamination Behavior of Carbon Fiber/Epoxy Composites

被引:9
作者
Low, Kean Ong [1 ,2 ]
Johar, Mahzan [3 ]
Israr, Haris Ahmad [1 ]
Gan, Khong Wui [4 ,5 ]
Rahimian Koloor, Seyed Saeid [6 ,7 ]
Petru, Michal [8 ]
Wong, King Jye [1 ]
机构
[1] Univ Teknol Malaysia, Sch Mech Engn, Fac Engn, Skudai 81310, Johor, Malaysia
[2] Multimedia Univ, Fac Engn & Technol, Ctr Adv Mat & Green Technol, Jalan Ayer Keroh Lama, Bukit Beruang 75450, Melaka, Malaysia
[3] Curtin Univ Malaysia, Fac Engn & Sci, Sarawak 98009, Malaysia
[4] Univ Southampton Malaysia, Sch Engn, Kota Ilmu Educ Iskandar, Iskandar Puteri 79200, Johor, Malaysia
[5] Univ Southampton, Sch Engn, Southampton SO17 1BJ, Hants, England
[6] Tech Univ Liberec TUL, Inst Nanomat Adv Technol & Innovat CXI, Studentska 2, Liberec 46117, Czech Republic
[7] Univ Putra Malaysia, Dept Aerosp Engn, Fac Engn, Serdang 43400, Selangor, Malaysia
[8] Tech Univ Liberec TUL, Studentska 2, Liberec 46117, Czech Republic
关键词
carbon; epoxy composite; Mode II delamination; cohesive zone model; displacement rate; fractography; INTERLAMINAR FRACTURE-TOUGHNESS; COHESIVE ZONE LENGTH; LOADING RATE; NUMERICAL-SIMULATION; GROWTH-BEHAVIOR; EPOXY; TEMPERATURE; FAILURE; I/II;
D O I
10.3390/polym13111881
中图分类号
O63 [高分子化学(高聚物)];
学科分类号
070305 ; 080501 ; 081704 ;
摘要
This paper studies the influence of displacement rate on mode II delamination of unidirectional carbon/epoxy composites. End-notched flexure test is performed at displacement rates of 1, 10, 100 and 500 mm/min. Experimental results reveal that the mode II fracture toughness G(IIC) increases with the displacement, with a maximum increment of 45% at 100 mm/min. In addition, scanning electron micrographs depict that fiber/matrix interface debonding is the major damage mechanism at 1 mm/min. At higher speeds, significant matrix-dominated shear cusps are observed contributing to higher G(IIC). Besides, it is demonstrated that the proposed rate-dependent model is able to fit the experimental data from the current study and the open literature generally well. The mode II fracture toughness measured from the experiment or deduced from the proposed model can be used in the cohesive element model to predict failure. Good agreement is found between the experimental and numerical results, with a maximum difference of 10%. The numerical analyses indicate crack jump occurs suddenly after the peak load is attained, which leads to the unstable crack propagation seen in the experiment.
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页数:18
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