首页> 外文会议>4th International Conference of the Engineering Integrity Society, 4th, Apr 10-12, 2000, Cambridge >Methodology for Modelling the Short Crack Fatigue Behaviour of Al-SiC MMCs
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Methodology for Modelling the Short Crack Fatigue Behaviour of Al-SiC MMCs

机译:Al-SiC MMC的短裂纹疲劳行为建模方法

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The objective of this study is to develop a computational modelling methodology for the fatigue crack growth behaviour of: (1) a forged 2124 Al reinforced with 17% SiC particles and (2) a cast 359 Al reinforced with 20% SiC particles. In particular, the focus of this work is on correlating local crack tip driving force conditions of an initial short crack with an experimental long crack growth rate curve, using crack closure. A defect tolerant approach is assumed. The crack tip is modelled using the finite element method, and the correlating parameter, ΔJ_(eff) (the effective range of the J-integral), is calculated. The material is assumed to be homogenous with the macroscale properties of the metal matrix composite, (MMC), for modelling purposes. An effective crack growth rate curve is calculated, and the ΔJ is used to obtain the crack growth increment per cycle. The method is repeated with the new crack size until the entire crack growth rate curve for the initial short crack is obtained. Crack growth rate curves for different stress levels and initial defect sizes are presented. Predicted S-N curves, obtained from the crack growth rate curves for a loading ratio of R=0.1, are compared with experimental results for each of the particulate reinforced MMCs. A good agreement with experimental results is obtained for an appropriate choice of defect size. Finally the method was validated by comparing the results on a Kitagawa diagram with those of the R-curve method, for the Al 2124 MMC.
机译:这项研究的目的是为以下情况的疲劳裂纹扩展行为开发一种计算模型方法:(1)用17%SiC颗粒增强的锻造2124 Al和(2)用20%SiC颗粒增强的铸造359 Al。尤其是,这项工作的重点是使用裂纹闭合技术将初始短裂纹的局部裂纹尖端驱动力条件与实验长裂纹生长速率曲线相关联。假定了一种容错方法。使用有限元方法对裂纹尖端进行建模,并计算相关参数ΔJ_(eff)(J积分的有效范围)。出于建模目的,假定该材料与金属基复合材料(MMC)的宏观特性均质。计算有效的裂纹扩展速率曲线,并使用ΔJ来获得每个周期的裂纹扩展增量。以新的裂纹尺寸重复该方法,直到获得初始短裂纹的完整裂纹扩展速率曲线。给出了不同应力水平和初始缺陷尺寸下的裂纹扩展速率曲线。对于每一个颗粒增强的MMC,将从裂纹扩展速率曲线(载荷比为R = 0.1)获得的预测S-N曲线与实验结果进行比较。对于缺陷尺寸的适当选择,可以获得与实验结果的良好一致性。最后,通过将Kitagawa图上的结果与R曲线方法的结果进行比较,对Al 2124 MMC进行了验证。

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