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A centrally cracked thin circular disk, part I: 3D elastic-plastic finite element analysis

机译:中心裂纹的薄圆盘,第一部分:3D弹塑性有限元分析

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A full field solution, based on small deformation, three-dimensional elastic-plastic finite element analysis of the centrally cracked thin disk under mode I loading has been performed. The solution for the stresses under small-scale yielding and locally fully plastic state has been compared with the HRR plane stress solution. At the outside of the 3D zone, within a distance of r sigma(o)/J = 18, HRR dominance is maintained in the presence of a significant amount of compressive stress along the crack flanks. Ahead of this region, the HRR field overestimate the stresses. These results demonstrate a completely reversed state of stress in the near crack front compared to that in the plane strain case. The combined effect of geometry and finite thickness of the specimen on elastic-plastic crack tip stress field has been explored. To the best of our knowledge, such an attempt in the published literature has not been made yet. For the qualitative assessment of the results some of the field parameters have been compared to the available experimental results of Chiang and Hareesh (1988). Under mixed mode loading, the dominance of the elastic K-field outside the elastic-plastic region has been demonstrated at the load level at which the crack extension experiment has been performed in the thin disk. At this load level the extents of yielding are about four sheet thickness under mode I loading and about five to seven sheet thicknesses under mixed mode I and II. These extents of plastic zones are smaller than the crack length but not much smaller. In the mode I analysis, it has been demonstrated that in the elastic-plastic region, the elastic stress intensity factor, K, gives a fair estimate of the crack opening stress near the crack front at a distance of order 10(-2) in. On the basis of this analysis, the Linear Elastic Fracture Mechanics approach has been adopted in analyzing the fatigue crack extension experiments performed in the disk (Part II). (C) 1998 Elsevier Science Ltd. All rights reserved. [References: 32]
机译:基于小变形,在模式I载荷下对中心裂纹薄盘进行了三维弹塑性有限元分析,得到了一个全场解决方案。将小规模屈服和局部完全塑性状态下的应力解与HRR平面应力解进行了比较。在3D区域的外部,在r sigma(o)/ J = 18的距离内,在沿裂纹侧面存在大量压缩应力的情况下,可以保持HRR优势。在该区域之前,HRR字段高估了应力。这些结果表明,与平面应变情况相比,裂纹近端的应力完全相反。研究了试样的几何形状和有限厚度对弹塑性裂纹尖端应力场的综合影响。据我们所知,尚未在公开文献中进行这种尝试。为了对结果进行定性评估,已将一些现场参数与Chiang和Hareesh(1988)的可用实验结果进行了比较。在混合模式载荷下,已在薄盘上进行裂纹扩展实验的载荷水平下证明了弹塑性区域外弹性K场的优势。在此负荷水平下,在模式I加载下屈服程度约为4个板厚,在模式I和II混合模式下屈服程度约为5至7个板厚。这些塑性区的范围小于裂缝长度,但不小很多。在模式I分析中,已经证明,在弹塑性区域中,弹性应力强度因子K可以合理地估计出裂纹前沿附近裂纹开裂应力,距离为10(-2)。在此分析的基础上,采用线性弹性断裂力学方法分析了在圆盘上进行的疲劳裂纹扩展实验(第二部分)。 (C)1998 Elsevier ScienceLtd。保留所有权利。 [参考:32]

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