{"title":"MULTIPLE FATIGUE CRACK GROWTH MODELLING IN NONHOMOGENEOUS STRUCTURAL SYSTEMS USING THE DUAL BEM","authors":"H. C. Andrade, E. Leonel","doi":"10.2495/be410031","DOIUrl":null,"url":null,"abstract":"This study presents a numerical scheme for the fatigue crack growth modelling in plane nonhomogeneous structural systems. The structural domain is assumed as composed of piecewise homogeneous isotropic materials. The high-cycle fatigue case is assumed. Consequently, the linear elastic fracture mechanics theory is utilized. The mechanical behaviour is represented by the dual boundary element method (DBEM), in which singular and hypersingular integral equations are applied. The DBEM is an efficient and robust numerical technique for crack propagation analyses, especially due to the non-requirement of the domain mesh. This aspect enables the accurate representation of the elastic fields around the crack tip and simplifies the remeshing process during the crack propagation. The singular integrals are evaluated through the singularity subtraction method. Third degree polynomial transformation is utilized for improving the accuracy of near-singular integrals. The interface between adjacent materials is assumed as perfectly bonded and the sub-region BEM approach is utilized for representing the nonhomogeneous bodies. The Paris’ law is utilized for determining the crack growth rate. The stress intensity factors are assessed by the J-integral and the maximum circumferential stress theory is adopted for defining the crack propagation angle and the range of equivalent stress intensity factor. The structural life is determined by a special scheme, which is based on discrete crack increments. One application is presented to illustrate the efficiency of the proposed model in simulating the fatigue crack growth in multiple cracked structures.","PeriodicalId":208184,"journal":{"name":"Boundary Elements and other Mesh Reduction Methods XLI","volume":"396 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-09-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Boundary Elements and other Mesh Reduction Methods XLI","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2495/be410031","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
This study presents a numerical scheme for the fatigue crack growth modelling in plane nonhomogeneous structural systems. The structural domain is assumed as composed of piecewise homogeneous isotropic materials. The high-cycle fatigue case is assumed. Consequently, the linear elastic fracture mechanics theory is utilized. The mechanical behaviour is represented by the dual boundary element method (DBEM), in which singular and hypersingular integral equations are applied. The DBEM is an efficient and robust numerical technique for crack propagation analyses, especially due to the non-requirement of the domain mesh. This aspect enables the accurate representation of the elastic fields around the crack tip and simplifies the remeshing process during the crack propagation. The singular integrals are evaluated through the singularity subtraction method. Third degree polynomial transformation is utilized for improving the accuracy of near-singular integrals. The interface between adjacent materials is assumed as perfectly bonded and the sub-region BEM approach is utilized for representing the nonhomogeneous bodies. The Paris’ law is utilized for determining the crack growth rate. The stress intensity factors are assessed by the J-integral and the maximum circumferential stress theory is adopted for defining the crack propagation angle and the range of equivalent stress intensity factor. The structural life is determined by a special scheme, which is based on discrete crack increments. One application is presented to illustrate the efficiency of the proposed model in simulating the fatigue crack growth in multiple cracked structures.
提出了平面非均质结构系统疲劳裂纹扩展模型的数值格式。假设结构域是由分段均匀各向同性材料组成。假设高周疲劳情况。因此,采用了线弹性断裂力学理论。采用双边界元法(dual boundary element method, DBEM),采用奇异积分方程和超奇异积分方程来表示结构的力学行为。DBEM是一种有效的、鲁棒的裂纹扩展数值分析方法,特别是由于它不需要区域网格。这一方面能够准确地表示裂纹尖端周围的弹性场,简化了裂纹扩展过程中的网格划分过程。通过奇异减法求奇异积分。利用三次多项式变换提高了近奇异积分的精度。假设相邻材料之间的界面是完美结合的,并采用分区域边界元法来表示非均匀体。利用帕里斯定律确定裂纹扩展速率。应力强度因子采用j积分计算,采用最大周向应力理论确定裂纹扩展角和等效应力强度因子范围。结构寿命由一种基于离散裂纹增量的特殊方案确定。通过一个实例说明了该模型在模拟多裂纹结构疲劳裂纹扩展方面的有效性。