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Numerical analysis of quasi-static crack branching in brittle solids by a modified displacement discontinuity method

机译:修正位移不连续法对脆性固体准静态裂纹分支的数值分析

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摘要

Mechanism of quasi-static crack branching in brittle solids has been analyzed by a modified displacement discontinuity method. It has been assumed that the pre-existing cracks in brittle solids may propagate at the crack tips due to the initiation and propagation of the kink (or wing) cracks. The originated wing cracks will act as new cracks and can be further propagated from their tips according to the linear elastic fracture mechanics (LEFM) theory. The kink displacement discontinuity formulations (considering the linear and quadratic interpolation functions) are specially developed to calculate the displacement discontinuities for the left and right sides of a kink point so that the first and second mode kink stress intensity factors can be estimated. The crack tips are also treated by boundary displacement collocation technique considering the singularity variation of the displacements and stresses near the crack tip. The propagating direction of the secondary cracks can be predicted by using the maximum tangential stress criterion. An iterative algorithm is used to predict the crack propagating path assuming an incremental increase of the crack length in the predicted direction (straight and curved cracks have been treated). The same approach has been used for estimating the crack propagating direction and path of the original and wing cracks considering the special crack tip elements. Some example problems are numerically solved assuming quasi-static conditions. These results are compared with the corresponding experimental and numerical results given in the literature. This comparison validates the accuracy and applicability of the proposed method.
机译:通过改进的位移不连续性方法分析了脆性固体中准静态裂纹分支的机理。假定由于扭结(或机翼)裂纹的产生和传播,脆性固体中预先存在的裂纹可能会在裂纹尖端传播。根据线性弹性断裂力学(LEFM)理论,起源的机翼裂纹将充当新裂纹,并可从其尖端进一步传播。扭结位移不连续性公式(考虑了线性和二次插值函数)是专门开发的,用于计算扭折点左侧和右侧的位移不连续性,以便可以估算第一和第二模式扭结应力强度因子。考虑到裂纹尖端附近位移和应力的奇异性变化,也通过边界位移配置技术处理裂纹尖端。次级裂纹的扩展方向可以通过最大切向应力准则来预测。使用迭代算法来预测裂纹扩展路径,假设裂纹长度沿预测方向增加(已处理了直形和弯曲裂纹)。考虑到特殊的裂纹尖端元素,使用相同的方法来估计原始裂纹和翼形裂纹的裂纹扩展方向和路径。假设准静态条件,可以用数值方法解决一些示例问题。将这些结果与文献中给出的相应实验和数值结果进行比较。这种比较验证了所提出方法的准确性和适用性。

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