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A survey on multiaxial fatigue damage parameters under non-proportional loadings

机译:非比例载荷下的多轴疲劳损伤参数研究

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摘要

In this paper, several multiaxial fatigue damage parameters taking into account nonproportional additional hardening are reviewed. According to the way nonproportional additional hardening is considered in the model, the damage parameters are classified into 2 categories: (1) equivalent damage parameters and (2) direct damage parameters. The equivalent damage parameters usually define a nonproportional coefficient to consider nonproportional additional cyclic hardening, and make a combination of this nonproportional coefficient with stress and/or strain quantities to calculate the equivalent damage parameters. In contrast, the direct damage parameters are directly estimated from the stress and strain quantities of interest. The accuracy of 4 multiaxial fatigue damage parameters in predicting fatigue lifetime is checked against about 150 groups of experimental data for 10 different metallic materials under multiaxial fatigue loading. The results revealed that both Itoh's model, one of equivalent damage parameters, and Susmel's model, which belong to direct damage parameters, could provide a better correlation with the experimental results than others assessed in this paper. So direct damage parameters are not better than the equivalent damage parameters in predicting fatigue lifetime.
机译:在本文中,考虑了非比例附加硬化的几个多轴疲劳损伤参数。根据模型中考虑非比例附加硬化的方式,将损伤参数分为两类:(1)等效损伤参数和(2)直接损伤参数。等效损伤参数通常定义非比例系数,以考虑非比例附加循环硬化,并将该非比例系数与应力和/或应变量组合起来以计算等效损伤参数。相反,直接损伤参数是直接从感兴趣的应力和应变量中估计的。针对多轴疲劳载荷下10种不同金属材料的约150组实验数据,检查了4个多轴疲劳损伤参数在预测疲劳寿命中的准确性。结果表明,同等损伤参数之一的Itoh模型和属于直接损伤参数的Susmel模型都可以比本文评估的其他模型提供更好的与实验结果的相关性。因此,在预测疲劳寿命时,直接损伤参数并不比等效损伤参数好。

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  • 作者单位

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    Department of Civil and Structural Engineering, The University of Sheffield, Sheffield SI 3JD, UK;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

    Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

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  • 正文语种 eng
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  • 关键词

    direct damage parameters; equivalent damage parameters; multiaxial fatigue; nonproportional additional hardening;

    机译:直接损伤参数;等效损伤参数;多轴疲劳非比例附加硬化;

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