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Strain rate-dependent deformation behaviors of multi-layer carbon fiber reinforced polymer laminates

机译:多层碳纤维增强聚合物层压板的应变率依赖性变形行为

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摘要

This paper focuses on the contributions of diversities of strain rate and orientations for aggravating the diversities of micro failure behaviors on carbon fiber reinforced polymer (CFRP) laminates. A miniature horizontal type tensile tester is employed to conduct experiments with strain rate ranging from 2.6 x 10(-6) s(-1) to 2.6 x 10(-3) s(-1). The CFRP laminates are obtained based upon a thermoset toughened epoxy matrix (termed CF/Epoxy) with ply orientations of (0 degrees/0 degrees) and (0 degrees/90 degrees). Significant differences in deformation behaviors of CFRP laminates are determined through tests. The study clearly reveals the strain rate-dependent deformation modes of CFRP laminates, involving pure fiber fracture, epoxy crack with stepped surface and interface failure with residual voids, determines the "low-high-low" variation tendency of Young's modulus and strength as a function of strain rate. Ply orientation-dependent differences in deformation behaviors are also investigated via severe interfacial shearing effect. A unified model consisted of four deformation modes to is clarified to analyze the complexity of CFRP laminates failure mechanism.
机译:本文研究了应变率和取向的差异对碳纤维增强聚合物(CFRP)层合板微观破坏行为差异的影响。采用小型卧式拉伸试验机进行试验,应变率范围为2.6x10(-6)s(-1)至2.6x10(-3)s(-1)。CFRP层板是基于热固性增韧环氧树脂基体(称为CF/环氧树脂)获得的,层板方向为(0度/0度)和(0度/90度)。通过试验确定了碳纤维复合材料层合板变形行为的显著差异。该研究清楚地揭示了CFRP层板的应变率相关变形模式,包括纯纤维断裂、带有阶梯表面的环氧树脂裂纹和带有残余孔隙的界面失效,确定了杨氏模量和强度随应变率的“低-高-低”变化趋势。此外,还通过严重的界面剪切效应,研究了层取向对变形行为的影响。为了分析碳纤维布层合板破坏机理的复杂性,建立了由四种变形模式组成的统一模型。

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