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Modeling of fatigue crack growth under high-low sequence loading

机译:高低序列载荷下疲劳裂纹扩展的建模

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The fatigue crack growth behavior of one compact tension specimen of 16MnR steel under high-low sequence loading was investigated. The symmetric half finite element model under plane-stress state was used to calculate the elastic-plastic stress-strain responses, in which the Armstrong-Frederick type cyclic plasticity model was implemented as a user material subroutine UMAT of ABAQUS. A recently developed dynamic crack growth model was used to simulate the effects of high loading step on the successive low loading step. The detailed evolution process of the crack closure and cyclic plastic zone within the retardation region of fatigue crack growth was obtained. The extend of the crack closure, the size of cyclic plastic zone and the stress gradient have significant influence on the fatigue crack growth rate. The predicted fatigue crack growth rate is in good agreement with the experimental data.
机译:研究了16MnR钢的一个紧凑拉伸试样在高-低序载荷下的疲劳裂纹扩展行为。使用平面应力状态下的对称半有限元模型来计算弹塑性应力-应变响应,其中将Armstrong-Frederick型循环可塑性模型实现为ABAQUS的用户材料子例程UMAT。最近开发的动态裂纹扩展模型用于模拟高负荷步骤对连续低负荷步骤的影响。获得了疲劳裂纹扩展延迟区内裂纹闭合和循环塑性区的详细演化过程。裂纹闭合的扩展,循环塑性区的大小和应力梯度对疲劳裂纹的扩展速率有重要影响。预测的疲劳裂纹扩展速率与实验数据吻合良好。

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