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Life prediction based on biaxial fatigue crack growth simulated in different microstructures modeled by using Voronoi-polygons

机译:基于双轴疲劳裂纹生长模拟的voronoi-多边形模拟不同微结构模拟的寿命预测

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Fatigue life is significantly affected by the crack growth behavior that depends on the material microstructure as well as the stress biaxiality. By considering such effects of microstructure and stress state on crack growth, a methodology to predict failure life in biaxial fatigue of materials with different microstructures was proposed in the present work. For more appropriate modeling, an aggregate of Voronoi-polygons was adopted to express microstructural features of polycrystalline materials. In the microstructure modeled by an aggregate of Voronoi-polygons, the crack initiation was quantitatively analyzed by considering the slip deformation on slip plane which is randomly set in each Voronoi-polygon. The algorithm for the crack growth was established as a competition between the growth by crack coalescences and the propagation of a dominant crack as a single crack. The coalescence growth under the assumed criteria was also taken into account among initiated and/or propagating cracks during the whole fatigue process. The failure life was statistically predicted based on the crack growth behavior simulated for forty distinct microstructural configurations, which were formed by generating different combinations of randomized shapes of Voronoipolygons for the same material. By applying the proposed analytical procedure, simulations were conducted according to the same conditions as experimental ones in fatigue tests, which had been carried out under axial, torsional and combined loading modes by using circumferentially-notched specimens of pure copper, medium carbon steel, and (α+β) and β titanium alloys. In this case, forty different failure-lives were obtained for each combination of material and loading mode. It was revealed that the failure lives observed in experiments were almost covered by the life-ranges between the minimum and the maximum lives given in simulation. It was also clarified that a dispersion of simulated lives was found to be larger at higher stress level.
机译:疲劳寿命受到裂缝生长行为的显着影响,这取决于材料微观结构以及应力双轴性。通过考虑微观结构和应力状态对裂缝生长的这种影响,提出了一种在本作工作中提出了一种预测具有不同微观结构的材料的双轴疲劳失效寿命的方法。为了更合适的建模,采用了voronoi-多边形的聚集体来表达多晶材料的微观结构特征。在由voronoi-多边形的聚集体建模的微观结构中,通过考虑在每个voronoi-polygon中随机设置的滑移平面上的滑移变形来定量分析裂纹开始。裂缝增长的算法被建立为裂缝聚合的生长与主要裂缝作为单一裂缝的繁殖之间的竞争。在整个疲劳过程中,还考虑了假定标准下的聚结生长。基于用于四十个不同的微观结构构造的裂纹生长行为,在统计上预测失败寿命,其通过为同一材料产生不同组合而形成的不同组合而形成。通过应用所提出的分析程序,根据与疲劳试验中的实验试验相同的条件进行模拟,该试验是通过使用纯铜,中碳钢的圆周缺口和组合的加载方式在轴向,扭转和组合的加载模式下进行。 (α+β)和β钛合金。在这种情况下,为每个材料和装载模式的组合获得了40个不同的失败。据透露,在实验中观察到的失败生命几乎被最小和最大寿命之间的寿命范围覆盖。还阐明了仿真生命的分散在较高的应力水平下被发现更大。

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