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Effect of Characteristic Parameters of Exponential Cohesive Zone Model on Mode Ⅰ Fracture of Laminated Composites

机译:指数粘结带模型特征参数对层合复合材料Ⅰ型断裂的影响。

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Delamination is a particularly dangerous damage mode of high performance laminated composites. In order to describe the composites ductile cracking and its progressive evolution accurately, the adjusted exponential cohesive zone model (CZM) is adopted, which correlates the tensile traction with the corresponding interfacial separation along the fracturing interfacial zone. At first the adjusted exponential CZM is used to simulate the Mode Ⅰ delamination of the standard double cantilever beam (DCB). The simulated results are in good agreement with the corrected beam theory and the corresponding experimental results. Then in order to research how the interfacial properties influence the Mode Ⅰ fracture, the interfacial strength and the critical energy release rate are studied. The main results are obtained as follows. The interfacial strength plays a crucial role in the laminated composites delamination onset, and it affects the peak load significantly if there is not a pre-crack. Once the delamination propagation begins to occur in the laminated composites, the responses of the load-displacement plots are relatively insensitive to the interfacial strength, and only the critical energy release rate is of critical importance. Furthermore, the peak load increases with the increase of the critical energy release rate and interfacial strength.
机译:分层是高性能层压复合材料特别危险的损坏方式。为了准确地描述复合材料的韧性开裂及其发展过程,采用了调整后的指数内聚区模型(CZM),该模型将拉伸牵引力与沿断裂界面区域的相应界面间距相关联。首先,将调整后的指数CZM用于模拟标准双悬臂梁(DCB)的模式Ⅰ分层。仿真结果与修正梁理论及相应的实验结果吻合良好。为了研究界面性质如何影响Ⅰ型断裂,研究了界面强度和临界能量释放率。主要结果如下。界面强度在层压复合材料的脱层开始中起着至关重要的作用,如果没有预裂化,它会显着影响峰值载荷。一旦分层复合材料中开始发生分层传播,载荷-位移图的响应对界面强度就变得相对不敏感,并且只有临界能量释放速率才是至关重要的。此外,峰值载荷随着临界能量释放速率和界面强度的增加而增加。

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