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首页> 外文期刊>Journal of Reinforced Plastics and Composites >A 3D micromechanical energy-based creep failure criterion for high-temperature polymer-matrix composites
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A 3D micromechanical energy-based creep failure criterion for high-temperature polymer-matrix composites

机译:基于3D微机械能的高温聚合物基复合材料蠕变破坏准则

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In the present study, a generalized three-dimensional (3D) energy-based criterion for the creep failure of viscoelastic materials is developed. Unlike the existing approaches which are restricted to uniaxial loading, the proposed criterion can predict failure under any combination of loads. This criterion is then incorporated into a simplified unit cell micromechanical model to predict the time-delayed failure of unidirectional polymer-matrix composites at elevated temperatures. 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 matrix time-dependent failure due to creep is a localized phenomenon. The micromechanical model is also used to estimate the ultimate strength of the constituents from the knowledge of the allowable strengths of the unidirectional composite in the principal material directions. The obtained creep failure stresses are found to be in reasonable agreement with the experimental data particularly for the 90° unidirectional laminate, where failure is totally matrix dominated.
机译:在当前的研究中,为粘弹性材料的蠕变破坏建立了一个基于三维(3D)能量的通用准则。与限制于单轴载荷的现有方法不同,所提出的标准可以预测在任何载荷组合下的破坏。然后将此标准合并到简化的晶胞微力学模型中,以预测高温下单向聚合物-基质复合材料的时间延迟失效。本研究中使用的复合材料为T300 / 934,适用于航空航天应用中的高温条件。使用微力学可以更准确地了解复合材料的失效机理,特别是在高温下,其中聚合物-基质复合材料的一般性能由基体粘弹性控制,而基体时间相关的因蠕变引起的破坏是局部现象。微观力学模型还用于从单向复合材料在主要材料方向上的允许强度的知识来估计成分的极限强度。发现获得的蠕变破坏应力与实验数据合理吻合,特别是对于90°单向层压板,其中破坏完全由基体主导。

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