Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5021315 | Composites Part B: Engineering | 2017 | 41 Pages |
Abstract
Obvious R-curve behavior exists in multidirectional carbon fiber reinforced polymers (CFRP) laminates under mode I loading, in which the plateau fracture toughness represents the steady-state delamination growth behavior. By decomposing the fracture toughness into the fracture work for pure delamination at the interface and that for the intra-ply damage of adjacent layers, a mechanism-based correlation between the plateau value of interface mode I fracture toughness in multidirectional laminates and the interface angle and/or the two angles of the fiber orientations of the two layers surrounding the crack tip was developed, which is an explicitly interface-dependent formula. Static tests were performed on six types of DCB specimen with different interfaces. The analytical calculations agreed well with the experimental data, verifying the proposed correlation. The intra-ply damage and fiber bridging during delamination along different interfaces were evaluated, which provides a justification for the proposed model.
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Authors
Libin Zhao, Yana Wang, Jianyu Zhang, Yu Gong, Zizi Lu, Ning Hu, Jifeng Xu,