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Abaqus implementation of extended finite element method using a level set representation for three-dimensional fatigue crack growth and life predictions

机译:使用水平集表示的Abaqus扩展有限元方法的三维疲劳裂纹扩展和寿命预测

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摘要

A three-dimensional extended finite element method (X-FEM) coupled with a narrow band fast marching method (FMM) is developed and implemented in the Abaqus finite element package for curvilinear fatigue crack growth and life prediction analysis of metallic structures. Given the level set representation of arbitrary crack geometry, the narrow band FMM provides an efficient way to update the level set values of its evolving crack front. In order to capture the plasticity induced crack closure effect, an element partition and state recovery algorithm for dynamically allocated Gauss points is adopted for efficient integration of historical state variables in the near-tip plastic zone. An element-based penalty approach is also developed to model crack closure and friction. The proposed technique allows arbitrary insertion of initial cracks, independent of a base 3D model, and allows non-self-similar crack growth pattern without conforming to the existing mesh or local remeshing. Several validation examples are presented to demonstrate the extraction of accurate stress intensity factors for both static and growing cracks. Fatigue life prediction of a flawed helicopter lift frame under the ASTERIX spectrum load is presented to demonstrate the analysis procedure and capabilities of the method.
机译:在Abaqus有限元软件包中开发并实现了三维扩展有限元方法(X-FEM)和窄带快速行进方法(FMM),用于曲线疲劳裂纹扩展和金属结构寿命预测分析。给定任意裂纹几何的水平集表示形式,窄带FMM提供了一种更新其不断发展的裂纹前沿的水平集值的有效方法。为了捕获塑性引起的裂纹闭合效应,采用了动态分配高斯点的单元划分和状态恢复算法,以有效整合近端塑性区中的历史状态变量。还开发了基于元素的惩罚方法来模拟裂纹闭合和摩擦。所提出的技术允许独立于基本3D模型的任意初始裂纹的插入,并且允许不符合现有网格或局部重新网格化的非自相似裂纹扩展模式。给出了几个验证示例,以演示提取静态裂纹和正在增长的裂纹的准确应力强度因子的方法。提出了有缺陷的直升机举升架在ASTERIX频谱载荷下的疲劳寿命预测,以证明该方法的分析过程和功能。

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