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PROGRESSIVE FAILURE ANALYSIS OF GLASS/EPOXY COMPOSITES AT LOW TEMPERATURES

机译:低温下玻璃/环氧树脂复合材料的逐步破坏分析

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Because of applications of composites in space and in low temperature equipment, low temperature mechanical properties of glass fiber-reinforced epoxy have to be assessed. Experimental or analytical investigation on the tensile failure behavior of glass/epoxy laminated composite with/or without stress concentration subjected to thermo-mechanical static loadings at low temperatures has not been done yet. In the present work, a model was developed to perform the progressive failure analysis of quasi isotropic composite plates at low temperatures. The initial failure load is calculated by means of an elastic stress analysis. The load is increased step by step. For each given load, the stresses are evaluated and the appropriate failure criterion is applied to inspect for possible failure. For the failed element, material properties are modified according to the failure mode using a non-zero stiffness degradation factor. Then, the modified Newton-Raphson iteration is carried out until convergence is reached. This analysis is repeated for each load increment until the final failure occurs and the ultimate strength is determined. The present method yields results in a reasonable agreement with the experimental data at room temperature and -60°C. The effect of low temperature on the failure mechanism of the plates was also determined.
机译:由于复合材料在空间和低温设备中的应用,必须评估玻璃纤维增​​强环氧树脂的低温机械性能。尚未进行对玻璃/环氧树脂层压复合材料在低温下承受热机械静态载荷和/或无应力集中的拉伸破坏行为的实验或分析研究。在目前的工作中,开发了一个模型来在低温下对准各向同性复合材料板进行渐进式失效分析。初始破坏载荷通过弹性应力分析计算。负载逐步增加。对于每个给定的负载,评估应力并应用适当的破坏准则来检查可能的破坏。对于失效元素,使用非零刚度退化因子根据失效模式修改材料属性。然后,执行修改后的牛顿-拉夫森迭代,直到达到收敛为止。对每个载荷增量重复此分析,直到发生最终破坏并确定极限强度为止。本方法产生的结果与室温和-60℃下的实验数据合理吻合。还确定了低温对板破坏机理的影响。

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