Mixed-mode fracture of adhesively bonded CF/epoxy composite joints

被引:19
|
作者
Daghyani, HR [1 ]
Ye, L [1 ]
Mai, YW [1 ]
机构
[1] UNIV SYDNEY, DEPT MECH & MECHATRON ENGN, CTR ADV MAT TECHNOL, SYDNEY, NSW 2006, AUSTRALIA
关键词
adhesive joints; mixed-mode fracture; carbon fibre/epoxy composite; bond thickness; strain energy release rate; rubber-modified epoxy;
D O I
10.1177/002199839603001104
中图分类号
TB33 [复合材料];
学科分类号
摘要
Mixed-mode fracture behaviour of adhesively bonded CF/Epoxy composite joints was studied using a rubber-modified epoxy (Araldite(R) GY260) as the adhesive. Fixed-ratio mixed-mode specimens (G(I)/G(II) = 4/3) were applied in the experiments. Composite adherends were manufactured from carbon fibre/epoxy (5128 T300 BASF) prepreg. The global mixed-mode fracture energy, G(c) of the joints with different bond thickness, t, was evaluated using compliance calibration obtained from the experiments, beam theory and finite element analysis. The crack path along the bond line in the adhesive joints was investigated using optical microscopy. It was found that G(c) was dependent on both the bond thickness and the actual crack path in the joints. G(c) increased mildly from thin bonds (t < 100 mu m) to a plateau value for larger bond thickness (t > 100 mu m). For poor bonding between the adhesive and the composite adherends, interfacial crack propagation was observed for very thin bonds with alternating crack jumping from one interface to another across the bond line. The crack propagated almost at one interface for large bonds with occasional kinking. However, for strong interfacial bonding, the crack was deviated from the mode-I precrack towards the composite adherend and propagated cohesively in the composite layer. Scanning electron microscopy on the fracture surfaces showed different morphology depending on the interfacial bonding between the adhesive and the composite adherend.
引用
收藏
页码:1248 / 1265
页数:18
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