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Dynamic compressive response and failure behaviour of CFRP composites at high strain rates

机译:高应变率下CFRP复合材料的动态压缩响应及失效行为

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A type of quasi-isotropic carbon/epoxy composites was prepared. In order to study the dynamic mechanical properties of composites, the compressive specimens were investigated in the normal direction, as well as in the in-plane direction at different strain rates by Hopkinson pressure bar (SHPB) technique. The macro- and micro-fracture morphology of the damaged specimens was obtained utilizing the scanning electron microscope (SEM). The experimental results showed that the dynamic stress-strain behaviour can be significantly affected by the strain rates. As the strain rates increased, the maximum strength and maximum modulus increased, the ultimate strain reduced. The compressive strength and the ultimate strain in the in-plane direction are obviously lower than that in the normal direction. The main way of the dynamic compressive failures in the normal direction is shear failure due to the brittle fracture of the fibre. Interfacial crack and delamination can be produced in the in-plane direction.
机译:制备一种拟种各向同性碳/环氧复合材料。为了研究复合材料的动态力学性能,在正常方向上研究压缩试样,以及Hopkinson压力棒(SHPB)技术的不同应变速率的面内方向。利用扫描电子显微镜(SEM)获得损坏标本的宏观和微骨折形态。实验结果表明,动态应力 - 应变行为可以受到应变率的显着影响。随着应变率增加,最大强度和最大模量增加,最终应变降低。面内方向上的抗压强度和极限应变显然低于正常方向的抗压强度。由于纤维的脆性骨折,正常方向上的动态压缩故障的主要方式是剪切失效。可以在面内方向上产生界面裂缝和分层。

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