材料科学
复合材料
抗弯强度
断裂韧性
三点弯曲试验
极限抗拉强度
复合数
弯曲
断裂力学
复合材料层合板
脆性
作者
Jianqiang Wang,Jinfei Cao,Xiaofa Yang,Xiao Hu,Peng Lü,Feng Jin
标识
DOI:10.1016/j.engfracmech.2022.108641
摘要
Fracture of notched Specimens of laminar glass fiber reinforced composite is quasi-brittle and with noticeable delamination crack growth around the notch tip, as indicated by the non-linear load–deflection curve close to the peak fracture load. In order to analyze the fracture performance of the composite with highly heterogeneous and anisotropic microstructures, the boundary effect model (BEM) considering the composite layered structures and damage along and perpendicular to the notch was adopted in this study. Around 90 notched three-point bending specimens with the span from 40 to 90 mm, plate thickness around 10 mm, the initial notch depth from 3 to 6 mm were tested and the maximum load Pmax values were recorded. The average fiber ply or layer thickness Cch was the characteristic microstructure modelled by BEM for both the crack-tip damage zone length (crack-bridging) and width (delamination). Both the tensile strength ft and fracture toughness KIC were determined from the notched bending tests. Direct tensile tests were also conducted and the measured tensile strength ft was close to the measurement from the three-point bending tests with the relative error < 6 %.
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