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A microscopic elasto-plastic damage model for characterizing transverse responses of unidirectional fiber-reinforced polymer composites

机译:一种微观弹塑性损伤模型,用于表征单向纤维增强聚合物复合材料的横向响应

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摘要

A phenomenological-based micromechanical method, comprising the coupling of the matrix constitutive model and the cohesive zone (CZM) model at fiber-matrix interfaces, is presented to investigate the mechanical behaviors of unidirectional (UD) fiber-reinforced polymer (FRP) composites subjected to transverse tension and compression. The key point of this method is the establishment of a novel elasto-plastic damage constitutive model using a fracture plane based yield criterion. Both plastic deformation and progressive failure procedure is incorporated in the implicit simulation. Special focus is given to the determination of the input values of constituent material properties, suggesting that directly using the macroscopic matrix properties to characterize the mechanical responses at the microscale level may bring large discrepancies in homogenized stress-strain responses of UD composites. A parametrical study is also carried out to calibrate cohesive parameters. The numerical results, in good agreement with experimental measurements, clearly reveal the damage scenarios and the dominant failure mechanisms. It can be concluded that the debonding of the fiber-matrix interfaces is responsible for the ultimate transverse tensile strength, while compression failure is governed by two possible modes, i.e. matrix compressive failure if matrix failure firstly occurs, and matrix tensile and interface debonding failure when debonding initiates first. Besides, the distribution of fracture plane angles in matrix is examined to further validate the predictive capacity of the proposed model.
机译:提出了一种基于现象的微机械方法,包括纤维 - 基质接口的基质本构模型和粘性区(CZM)模型的偶联,以研究单向(UD)纤维增强聚合物(FRP)复合材料的机械行为横向张力和压缩。该方法的关键点是使用基于裂缝平面的屈服标准建立新的弹性塑料损伤本构模型。塑性变形和渐进式故障程序都包含在隐式模拟中。特别焦点对组成材料特性的输入值的测定,表明直接使用宏观​​基质特性以表征微尺度水平的机械响应可以在UD复合材料的均质应力 - 应变响应中引起大的差异。还进行了参数研究以校准内聚参数。数值结果与实验测量良好,清楚地揭示了损坏的情景和主导失败机制。可以得出结论,纤维 - 矩阵接口的剥离负责最终的横向拉伸强度,而压缩失败由两种可能的模式控制,即矩阵压缩失败,如果矩阵失败首先发生,而矩阵拉伸和接口剥离失败剥夺首先启动。此外,检查矩阵中的断裂平面角度的分布,以进一步验证所提出的模型的预测能力。

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