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Fatigue crack growth under variable -amplitude loading: Part Ⅰ -Model formulation in state-space setting

机译:变幅载荷下的疲劳裂纹扩展:第一部分-状态空间模型的建立

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This two -part paper presents formulation and validation of a non-linear dynamical model of fatigue crack growth in ductile alloys under variable-amplitude loading including single-cycle overloads, irregular sequences, and random loads. The model is formulated in the state-space setting based on the crack closure concept and captures the effects of stress overload and reverse plastic flow. The state variables of the model are crack length and crack opening stress. This paper, which is the first pat, presents formulation of the state-space model that can be restructured as an autoregressive moving average (ARMA) model for real-time applications such as health monitoring and life extending control. The second part is the companion paper that is dedicated to model validation with fatigue test data under different types of variable -amplitude and spectrum loading.
机译:这份由两部分组成的文章介绍了可变振幅载荷(包括单周期过载,不规则序列和随机载荷)下延性合金疲劳裂纹扩展的非线性动力学模型的制定和验证。该模型基于裂纹闭合概念在状态空间设置中建立,并捕获应力过载和反向塑性流动的影响。模型的状态变量是裂纹长度和裂纹张应力。本文是第一篇,介绍了状态空间模型的公式化,可以将其重构为自回归移动平均(ARMA)模型,用于实时应用,例如健康监控和寿命控制。第二部分是随附的论文,该论文专门针对不同类型的可变振幅和频谱负载下的疲劳测试数据进行模型验证。

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