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Mechanical behavior and damage kinetics of woven E-glass/vinylester laminate composites under high strain rate dynamic compressive loading: Experimental and numerical investigation

机译:高应变率动态压缩载荷下机织E-玻璃/乙烯基酯层压复合材料的力学行为和破坏动力学:实验和数值研究

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Split Hopkinson pressure bar (SHPB) is one of the most important and recognized apparatus used for characterizing the dynamic behavior of materials. In the first part of this study, the results from a series of SHPB tests on the woven composites are presented in this paper. The compressive material properties are determined by testing the [0 degrees/90 degrees](26) laminate systems from low to high strain rates. Samples of cubic geometry are tested in in-plane and out-of-plane direction. Preliminary compressive stress-strain vs. strain rates data obtained show that the dynamic material strength increases with increasing strain rates. The tests show a strong material sensitivity to dynamic loading. For in-plane tests, there is a transitional strain rate, reflecting the dependencies on strain rate observed in experiments. The results indicate that the stress-strain curves, maximum compressive stresses and strains evolve as strain rate changes. During the experiments, a high speed camera was used to determine the kinetics of damage. The specimens are mainly damaged in a crushing and shear failure mode under out-of-plane loading, as for in-plane test, the failure was dominated by fiber buckling and delamination. In the second part of this study, numerical models without damage are developed to investigate the validity of assumptions of compression Split-Hopkinson Pressure Bar technique. Abaqus software was used for the numerical simulation. The results obtained by numerical investigation of SHPB are compared with the in-plane and out-of-plane compression test of a woven composite. A good correlation was noted between the experimental and numerical results, which allows validate the numerical approach. (C) 2015 Elsevier Ltd. All rights reserved.
机译:霍普金森分体式压力棒(SHPB)是用于表征材料动态特性的最重要和公认的仪器之一。在本研究的第一部分中,本文介绍了一系列针对机织复合材料的SHPB测试结果。压缩材料的性能是通过测试[0度/ 90度](26)层压板系统从低应变率到高应变率来确定的。在平面内和平面外方向测试立方几何形状的样本。初步的压缩应力-应变对应变率数据表明,动态材料强度随应变率的增加而增加。测试表明,材料对动态载荷具有很强的敏感性。对于平面测试,存在一个过渡应变速率,反映了在实验中观察到的应变速率的依赖性。结果表明,应力应变曲线,最大压缩应力和应变随着应变率的变化而变化。在实验过程中,使用高速相机确定损坏的动力学。试样在平面外载荷下以破碎和剪切破坏模式受到破坏,在平面内测试中,破坏主要由纤维屈曲和分层引起。在本研究的第二部分中,开发了无损伤的数值模型以研究压缩斯普利特-霍普金森压杆技术假设的有效性。使用Abaqus软件进行数值模拟。通过SHPB数值研究获得的结果与机织复合材料的面内和面外压缩测试进行了比较。实验结果和数值结果之间存在良好的相关性,这可以验证数值方法。 (C)2015 Elsevier Ltd.保留所有权利。

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