首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part M. Journal of Engineering for the Maritime Environment >An improved constitutive model to predict fatigue crack growth rate under constant-amplitude loading with single and multiple overload
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An improved constitutive model to predict fatigue crack growth rate under constant-amplitude loading with single and multiple overload

机译:改进的本构模型预测单振幅和多过载等幅载荷下的疲劳裂纹扩展速率

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摘要

Fatigue crack growth under variable-amplitude loading is usually accompanied by the load interaction effect. One of the significant phenomena of load interaction effects is retardation induced by an overload or multiple overloads. To predict the fatigue crack growth rate under constant-amplitude loading with single and multiple overload, an improved constitutive model based on partial crack closure due to crack-tip plasticity is proposed in this paper. In this model, both the maximum stress intensity factor at crack opening level and the threshold value of effective stress intensity factor range are expressed as the explicit functions of stress ratio and the threshold stress intensity factor range when stress ratio is zero. It is assumed in the improved constitutive model that the crack closure level can rise due to a larger plastic zone resulting from the overload effect, and a modified coefficient based on the Wheeler model is introduced to correct the amount of the maximum stress intensity factor at crack opening level during the recovering period after an overload. By a cycle-by-cycle integration procedure, the fatigue crack growth rate under constant-amplitude loading with single and multiple overload is predicted quantitatively with this model. Comparison is made between the results of analytical predictions and experimental data and good agreements are found. This indicates that the proposed constitutive model is able to explain the load interaction effect under variable-amplitude loading.
机译:可变振幅载荷下的疲劳裂纹扩展通常伴随有载荷相互作用效应。负载相互作用效应的重要现象之一是过载或多次过载引起的延迟。为了预测等振幅载荷下单次和多次过载下的疲劳裂纹扩展速率,提出了一种基于裂纹尖端塑性的部分裂纹闭合本构模型。在该模型中,裂纹开放水平处的最大应力强度因子和有效应力强度因子范围的阈值均表示为应力比和应力比率为零时的阈值应力强度因子范围的显式函数。假设在改进的本构模型中,由于过载效应导致塑性区变大,裂纹闭合水平会上升,并基于Wheeler模型引入了修正系数,以修正裂纹处的最大应力强度因子的数量。过载后恢复期间的打开水平。通过逐周期积分程序,用该模型定量预测了在单振幅和多重过载的等幅载荷下的疲劳裂纹扩展速率。将分析预测的结果与实验数据进行比较,并找到良好的一致性。这表明所提出的本构模型能够解释变幅载荷下的载荷相互作用效应。

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