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Modeling Of Fatigue Crack Growth Of Stainless Steel 304l

机译:304l不锈钢疲劳裂纹扩展的建模

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An effort is made to predict the crack growth of the stainless steel 304L based on a newly developed fatigue approach. The approach consists of two steps: (1) elastic-plastic finite element (FE) analysis of the component; and, (2) the application of a multiaxial fatigue criterion for the crack initiation and growth predictions based on the outputted stress-strain response from the FE analysis. The FE analysis is characterized by the implementation of an advanced cyclic plasticity theory that captures the important cyclic plasticity behavior of the material under the general loading conditions. The fatigue approach is based upon the notion that a material point fails when the accumulated fatigue damage reaches a certain value and the rule is applicable for both crack initiation and growth. As a result, one set of material constants is used for both crack initiation and growth predictions. All the material constants are generated by testing smooth specimens. The approach is applied to Mode I crack growth of compact specimens subjected to constant amplitude loading with different R-ratios and two-step high-low sequence loading. The results show that the approach can properly model the experimentally observed crack growth behavior including the notch effect, the R-ratio effect, and the sequence loading effect. In addition, the early crack growth from a notch and the total fatigue life can be simulated with the approach and the predictions agree well with the experimental observations.
机译:基于新开发的疲劳方法,努力预测304L不锈钢的裂纹扩展。该方法包括两个步骤:(1)组件的弹塑性有限元(FE)分析; (2)基于有限元分析输出的应力-应变响应,将多轴疲劳准则应用于裂纹萌生和扩展预测。有限元分析的特点是实施了先进的循环可塑性理论,该理论捕获了材料在一般载荷条件下的重要循环可塑性行为。疲劳方法基于这样的观念:当累积的疲劳损伤达到一定值时,材料点会失效,并且该规则适用于裂纹萌生和扩展。结果,一组材料常数用于裂纹萌生和增长预测。所有材料常数都是通过测试光滑样品而产生的。该方法适用于在具有不同R比率和两步高-低序列载荷的恒定振幅载荷下的紧凑型试样的I型裂纹扩展。结果表明,该方法可以正确地模拟实验观察到的裂纹扩展行为,包括缺口效应,R比率效应和序列加载效应。此外,可以通过该方法模拟从缺口处开始的早期裂纹扩展和总疲劳寿命,并且预测结果与实验结果非常吻合。

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