Study of an On-Line Crack Compliance Technique for Residual Stress Measurement Using 2D Finite Element Simulations of Fatigue Crack Growth

S. Ismonov, S. Daniewicz
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引用次数: 1

Abstract

There are several methods available to measure residual stress fields present within a structural component. Recently a new so called on-line crack compliance technique has been proposed, which is based on linear elastic fracture mechanics. This experimental method uses incremental crack mouth opening displacements measured during fatigue crack growth testing to generate information on the existing residual stresses along the crack line. The present study employs two dimensional (2D) plane stress finite element simulations of fatigue crack growth from a cold worked hole to investigate the performance of this technique. Using the simulation results, the stress intensity factors due to the residual stress field normalized by the maximum applied stress intensity factor KIrs/KImax were obtained from the on-line crack compliance method. For validation, the J-integral approach was used to calculate KIrs/KImax values from fatigue crack growth simulations in an elastic material. The two methods generated nearly identical results. Fatigue crack growth was also simulated in an elastic-plastic material. Even though the stress intensity factor is not the appropriate crack tip characterizing technique for elastic-plastic material conditions, it is still investigated here to approximate the actual testing conditions, where plastic deformation near the crack tip is unavoidable. The KIrs/KImax solutions are presented for different cold work levels and applied loadings. Results indicate that the agreement between the elastic and elastic-plastic crack growth solutions is dependent on the maximum applied loading level, as might be expected.
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基于二维有限元模拟疲劳裂纹扩展的在线残余应力测量技术研究
有几种方法可用于测量存在于结构部件内的残余应力场。近年来提出了一种基于线弹性断裂力学的在线裂纹柔化技术。该实验方法利用疲劳裂纹扩展试验中测量的增量裂纹张开位移来生成沿裂纹线存在的残余应力信息。本研究采用二维平面应力有限元模拟冷加工孔的疲劳裂纹扩展,以研究该技术的性能。利用仿真结果,利用在线裂纹柔度法得到了由最大外加应力强度因子KIrs/KImax归一化的残余应力场引起的应力强度因子。为了验证,使用j积分方法计算弹性材料疲劳裂纹扩展模拟的KIrs/KImax值。这两种方法产生了几乎相同的结果。模拟了弹塑性材料的疲劳裂纹扩展。尽管应力强度因子不是弹塑性材料条件下裂纹尖端的合适表征技术,但本文仍在研究如何近似实际试验条件,因为裂纹尖端附近的塑性变形是不可避免的。KIrs/KImax解决方案适用于不同的冷加工水平和应用负载。结果表明,弹性和弹塑性裂纹扩展解之间的一致性取决于最大加载水平,正如预期的那样。
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