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A tensile impact apparatus for characterization of fibrous composites at high strain rates

机译:拉伸冲击装置,用于表征高应变率下的纤维复合材料

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A high rate tensile testing apparatus called "flying wedge" for testing fibrous composites at strain rates up to 10~3 s~(-1) has been described.R2000 glass/epoxy composite has been tested at a very low strain rate of 10~3 s~(-1) using the universal Instron tensile testing machine, and at high strain rates up to nearly 850s~(-1) using flying wedge. The results show significant increase in failure stress and reduction in failure strain for dynamic tests with respect to quasi-static experiments. While the reduction in failure strain fluctuates from 60 to 75 percent. the increase in failure strength varies from 300 to even 500 percent for different ply angles. Although, the results may be affected by the stress waves, which propagate through the parts of the testing machine on the impact, it is found that the stress wave's effects do not play a determinant role in this regard. The results indicate that the rate of the increase of stress versus strain rate slows down as ply angle increases. Scanning electron microscopy of the fracture surface of the specimens did not reveal significant difference between the failure mechanisms at low and high strain rates.
机译:已经描述了一种高速率的拉伸测试设备,称为“飞楔”,用于以高达10〜3 s〜(-1)的应变速率测试纤维复合材料。R2000玻璃/环氧树脂复合材料已经以非常低的10%的应变速率进行了测试使用通用Instron拉伸试验机3 s〜(-1),使用飞楔在高达850s〜(-1)的高应变速率下。结果表明,相对于准静态实验,动态测试的破坏应力显着增加,破坏应变减小。失效应变的减少从60%波动到75%。对于不同的帘布层角度,破坏强度的增加范围从300%到500%不等。尽管结果可能会受到应力波的影响,应力波会在冲击时通过测试机的各个部分传播,但发现应力波的影响在这方面没有决定性作用。结果表明,随着层板角度的增加,应力与应变率的增加速率降低了。样品的断裂表面的扫描电子显微镜没有显示出在低应变速率和高应变速率下的破坏机理之间的显着差异。

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