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A Micromechanics Model for Fatigue Life Prediction of Metal Matrix Composites

机译:预测金属基复合材料疲劳寿命的微力学模型

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摘要

In this paper, a cumulative damage model is described to predict the fatigue lift of unidirectional metla matrix composites under combined thermo-mechanical fatigue loading. The fatigue life prediction is based on the critical element model. A micromechanics model is used to predict the accumulation of damage in the form of fiber fractures, matrix plasticity and interfacial debonding. The fatigue life is estimated using a linear summation life fraction rule. In the present model, both the local stresses and strength of the constituents of the composite namely fiber, matrix and interface are considered. Results indicate that the predicted fatigue life of unidirectional MMCs agree well with the experimental data for a variety of composites. The model can predict the effects of test temperature, fiber volume fraction, loading frequency and thermomechanical fatigue (TMF) loading well.
机译:在本文中,描述了一种累积损伤模型来预测在热机械疲劳联合作用下单向金属基复合材料的疲劳强度。疲劳寿命预测基于关键要素模型。使用微力学模型来预测破坏的累积形式,包括纤维断裂,基质可塑性和界面剥离。使用线性求和寿命分数规则估算疲劳寿命。在本模型中,考虑了复合材料成分的局部应力和强度,即纤维,基体和界面。结果表明,单向MMC的预测疲劳寿命与多种复合材料的实验数据吻合良好。该模型可以很好地预测测试温度,纤维体积分数,加载频率和热机械疲劳(TMF)加载的影响。

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