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Numerical Simulation of Failure Behavior Under Impact Loading for Cylindrical Carbon Fiber Reinforced Polymer

机译:圆柱碳纤维增强聚合物冲击载荷下失效行为的数值模拟

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This study presents a prediction for the dynamic failure behavior of the carbonfiber reinforced polymer (CFRP) under impact loading. In the experiment, the splitHopkinson pressure bar (SHPB) test was conducted by using two types of cylindricalCFRP specimens. The commercial finite element analysis (FEA) software Abaquswas used for the analysis. In this study, we considered two types of failuremechanisms, a problem that mainly involves matrix-dominated failure and does notinvolve fiber breakage and a problem that involves fiber-dominated failure. To predictthe matrix-dominated failure, we adopted multi-scale analysis, which is a method thatcan carry out analysis at different scales. We considered the damage initiation criterionbased on continuum damage mechanics (CDM). This damage initiation criterion wasbased on the Christensen failure criterion. We simulated interfacial failure by usingcohesive zone modeling (CZM), which considers failure conditions in mixed mode. Inmicro-scale analysis, a two-dimensional periodic unit cell (PUC) was used and weconsidered CDM and CZM. Macro-scale analysis was conducted in the same way asin the SHPB experiments. To predict the fiber-dominated failure, simulation wascarried out using the Hashin damage theory. Parameters used in macro-scale analysiswere obtained from micro-scale analysis. Macro-scale analysis is currently conducted.
机译:这项研究提出了碳动态失效行为的预测 冲击载荷作用下的纤维增强聚合物(CFRP)。在实验中,分裂 霍普金森压力棒(SHPB)测试是通过使用两种类型的圆柱体进行的 CFRP标本。商业有限元分析(FEA)软件Abaqus 用于分析。在这项研究中,我们考虑了两种类型的失败 机制,这个问题主要涉及矩阵主导的故障,并不涉及 涉及光纤断裂以及涉及光纤占主导地位的故障的问题。预测 对于矩阵主导的失效,我们采用多尺度分析,这是一种方法 可以进行不同规模的分析。我们考虑了损害起始标准 基于连续损伤机制(CDM)。该损害起始标准为 根据克里斯滕森(Christensen)破坏准则。我们通过使用来模拟界面破坏 内聚区建模(CZM),它考虑了混合模式下的失效条件。在 微观分析,使用了二维周期性晶胞(PUC),我们 被认为是CDM和CZM。宏观分析的方法与 在SHPB实验中。为了预测光纤主导的故障,模拟是 使用Hashin损伤理论进行。宏观分析中使用的参数 从微观分析中获得。目前正在进行宏观分析。

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