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Mixed-Mode (I+II) Fracture Toughness and Rate Dependent Fracture Behavior of Interlayer-Toughened Composite Laminate

机译:混合模式(I + II)中间钢化复合层压板的裂缝韧性和速率依赖性断裂行为

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摘要

Mixed mode (I + II) fracture toughness of the interlayer-toughened composite laminates, T800H/3900-2 (Toray), which is a newly developed composite material having a tough 'interlayer' containing fine polyamide particles, was investigated over a very wide range of loading rate from static to impact The MMF (Mixed Mode Flexure) specimen and SHPB (Split Hopkinson Pressure Bar) system were employed for measuring the mixed mode fracture toughness under impact loading. The strain rate dependence of fracture behavior was also studied from both macro- and microscopic aspects to clarify the mesoscopic fracture mechanism of the material. The experimental results showed the crack path was inside the toughened interlayer during the initial stage of crack growth, however, it moved from the toughened interlayer to the carbon/epoxy base lamina during the propagation stage of crack growth. The mixed mode fracture toughness was sensitive to loading rate; the impact fracture toughness for the toughened interlayer was about 23 percent lower than the maximum value under static loading, and the impact fracture toughness for the carbon/epoxy base lamina was about 11 percent lower than the maximum value under static loading. The effects of mode mixture varied with loading rate for interlayer fracture, though they did not varied for base-lamina fracture. Microscopic observation showed that the fracture morphology was sensitive to loading rate.
机译:层间 - 增韧复合层压板的混合模式(I + II)裂缝韧性,T800H / 3900-2(TORAY),其是具有坚韧的“含有含有细聚酰胺颗粒的新开发的复合材料”,在非常宽的情况下研究采用静电冲击MMF(混合模式弯曲)标本和SHPB(分裂霍普金森压力棒)系统的加载速率范围用于测量冲击载荷下的混合模式断裂韧性。来自宏观和微观方面的裂缝行为的应变率依赖性,以阐明材料的介观骨折机制。实验结果表明,在裂纹生长的初始阶段期间,裂纹路径在韧性中间层内部在抗裂纹生长的初始阶段内。在裂纹生长的繁殖阶段,它从燃烧的中间层移动到碳/环氧基础薄膜。混合模式断裂韧性对装载速率敏感;韧性中间层的冲击断裂韧性比静态载荷下的最大值低约23%,碳/环氧基础薄片的冲击断裂韧性比静态载荷下的最大值低约11%。模式混合物的影响随着层间骨折的负载率而变化,但它们对底层裂缝没有变化。显微镜观察表明,骨折形态对装载速率敏感。

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