Please use this identifier to cite or link to this item: http://hdl.handle.net/123456789/28043
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dc.contributor.authorKean Ong Low-
dc.contributor.authorMahzan Johar-
dc.contributor.authorAun Naa Sung-
dc.contributor.authorMohd Nazri Mohd Nasir-
dc.contributor.authorSeyed Saeid Rahimian Koloor-
dc.contributor.authorMichal Petru-
dc.contributor.authorHaris Ahmad Israr-
dc.contributor.authorKing Jye Wong-
dc.contributor.author(UniKL MITEC)-
dc.date.accessioned2023-07-05T03:04:46Z-
dc.date.available2023-07-05T03:04:46Z-
dc.date.issued2023-07-05-
dc.identifier.urihttp://hdl.handle.net/123456789/28043-
dc.descriptionThis article is index by Scopus.en_US
dc.description.abstractMixed-mode delamination is one of the common failures of composites which has not been studied under low-impact loading. This paper studies the influence of displacement rate on mixed-mode I/II delamination of unidirectional carbon/epoxy composites. Single leg bending test is performed at displacement rates of 1, 10, 100, and 500 mm/min. Experimental results reveal that the mixed-mode I/II fracture toughness is invariant with the displacement rate. In addition, scanning electron micrographs shows that shear cusps are more obvious at 1, 10, and 100 mm/min. At 500 mm/min, significant matrix debris is noticed. Furthermore, the proposed three-dimensional rate-dependent fracture criterion is found to well predict the fracture toughness. Numerical simulation using cohesive zone model suggests that the lower numerical peak load is due to lower damage dissipated energy. In addition, the theoretical and numerical traction-separation responses show significant differences, which is also reflected in the numerical phase angle. This implies that the local mixed-mode ratio is not constant throughout the simulation process.en_US
dc.subjectCarbon/epoxy compositeen_US
dc.subjectCohesive zone modellingen_US
dc.subjectFractographyen_US
dc.subjectMixed-mode delaminationen_US
dc.subjectRate dependenceen_US
dc.titleDisplacement rate effects on mixed-mode I/II delamination of laminated carbon/epoxy compositesen_US
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