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Determination of the strain-energy release rate of a composite laminate under high-rate tensile deformation in fibre direction

机译:纤维方向高速拉伸变形下复合材料层合板应变能释放率的测定

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摘要

In order to successfully model design-critical impact loading events on laminated composite structures, the rate dependency of the composite material has to be correctly reflected. In this context, the rate-dependency of the strain-energy release rate for fibre tensile failure under high-rate loading conditions has not yet been satisfyingly explored. This study employed compact tension specimens consisting of IM7/8552 for dynamic testing on a split Hopkinson tension bar system. Data reduction was based on the area method. The obtained strain-energy release rate for testing under high-rate conditions was determined to G(Ic,dyn)(integral+) = 82.0 +/- 20.8kJ/m(2), exhibiting a salient drop compared to its counterpart obtained under quasi-static loading (G(Ic,Qs)(integral+) = 195.8 +/- 18.0kJ/m(2)). Analysis of the strain field surrounding the crack tip using digital image correlation (DIC) suggested a more extensive damage zone for testing under quasi-static than for high-rate loading. A fractographic analysis of the specimens did not indicate any pronounced difference in terms of fracture surface morphology across the two loading rate regimes.
机译:为了成功地对层压复合结构上的设计关键冲击载荷事件进行建模,必须正确反映复合材料的速率依赖性。在这种情况下,尚未令人满意地探索在高速率负荷条件下纤维拉伸断裂的应变能释放速率的速率依赖性。这项研究采用了由IM7 / 8552组成的紧凑型拉伸试样,用于在拆分的Hopkinson拉伸杆系统上进行动态测试。数据缩减基于面积法。将获得的用于高速率条件下测试的应变能释放速率确定为G(Ic,dyn)(integral +)= 82.0 +/- 20.8kJ / m(2),与在准条件下获得的对应物相比,其显着下降-静态载荷(G(Ic,Qs)(integral +)= 195.8 +/- 18.0kJ / m(2))。使用数字图像相关(DIC)对裂纹尖端周围的应变场进行分析的结果表明,在准静态条件下进行测试的损伤区域比在高速率载荷下更为广泛。样品的分形分析没有显示出在两种加载速率方案下的断裂表面形态方面的任何明显差异。

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