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A micromechanical approach for the prediction of the time-dependent failure of high temperature polymer matrix composites

机译:预测高温聚合物基复合材料时间相关失效的微力学方法

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摘要

In the present study, a novel micromechanical approach is introduced to study the time-dependent failure of unidirectional polymer matrix composites. The main advantage of the present micromechanical model lies in its ability to give closed-form solutions for the effective nonlinear response of unidirectional composites and to predict the material response to any combination of shear and normal loading. The creep failure criterion is expressed in terms of the creep failure functions of the viscoelastic matrix material. The micromechanical model is also used to calculate these creep failure functions from the knowledge of the creep behavior of the composite material in only transverse and shear loadings, thus eliminating the need for any further experimentation. The composite material used in this study is T300/934, which is suitable for service at high temperatures in aerospace applications. The use of micromechanics can give a more accurate insight into the failure mechanisms of the composite materials in particular at high temperatures where the general behavior of the polymer matrix composite is governed by matrix viscoelasticity and the time-dependent failure of the matrix is a localized phenomenon. The obtained creep failure stresses are found to be in reasonable agreement with the experimental data.
机译:在本研究中,一种新颖的微机械方法被引入来研究单向聚合物基复合材料的时间依赖性破坏。本微机械模型的主要优点在于,它能够为单向复合材料的有效非线性响应提供闭合形式的解,并能够预测材料对剪切和法向载荷的任意组合的响应。蠕变破坏准则以粘弹性基体材料的蠕变破坏函数表示。根据仅在横向和剪切载荷下复合材料的蠕变行为的知识,微机械模型也可用于计算这些蠕变破坏函数,从而无需进行任何进一步的实验。本研究中使用的复合材料是T300 / 934,它适​​合在航空航天应用中的高温下使用。使用微力学可以更准确地了解复合材料的破坏机理,特别是在高温下,在这种情况下,聚合物基复合材料的一般性能受基体粘弹性控制,基体的时间依赖性破坏是局部现象。发现获得的蠕变破坏应力与实验数据合理吻合。

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