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首页> 外文期刊>International Journal of Fatigue >Experimental and numerical investigation of mixed mode fatigue crack growth models in aluminum 6061-T6
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Experimental and numerical investigation of mixed mode fatigue crack growth models in aluminum 6061-T6

机译:铝6061-T6混合模式疲劳裂纹扩展模型的实验与数值研究

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摘要

Damage tolerance philosophy and safe life design principles are widely used for critical structural components, and in such cases, fatigue life prediction using the numerical techniques is essential. In the present work, mixed mode fatigue crack growth experiments are performed using the compact tension shear specimens made of Al 6061-T6 alloy for mode mixity angles of 30 degrees, 45 degrees, and 60 degrees. These experimental studies are supported by numerical and fractographic studies on the selected specimens. A three-parameter double exponential model for fitting the fatigue crack growth curves (crack length vs. the number of fatigue life cycles) is also proposed for both the mode I and mixed mode (I/II) loading conditions. Numerical prediction of mixed mode (I/ID fatigue life is carried out using the Paris' law in combination with various Delta K-eq models. The results of the present investigation show that highly satisfactory best fits to the scattered experimental data can be obtained with the help of the proposed double exponential model. The predicted life is compared with the experimental fatigue life using various measures of error. Based on the overall performance of the models during the entire crack growth regime, the results of the present investigation clearly show that Irwin's model and one of the Tanaka's model are consistently found to predict the mixed mode fatigue life close to the experimental data. Whereas, Richard's and Yan's models, again based on the overall performance, are found to be conservative models consistently for the prediction of the mixed mode fatigue life. These conclusions are verified with the published results.
机译:损伤容忍原理和安全寿命设计原则已广泛用于关键的结构部件,在这种情况下,使用数值技术预测疲劳寿命至关重要。在当前工作中,使用由Al 6061-T6合金制成的紧凑型拉伸剪切试样对模式混合角为30度,45度和60度进行了混合模式疲劳裂纹扩展实验。这些实验研究得到所选标本的数值和分形学研究的支持。还针对模式I和混合模式(I / II)加载条件,提出了用于拟合疲劳裂纹扩展曲线(裂纹长度与疲劳寿命周期数)的三参数双指数模型。混合模态(I / ID疲劳寿命的数值预测是使用巴黎定律和各种Delta K-eq模型进行的。本研究的结果表明,对于零散的实验数据,可以获得非常满意的最佳拟合)。在提出的双指数模型的帮助下,使用各种误差度量将预测寿命与实验疲劳寿命进行了比较,基于模型在整个裂纹扩展过程中的整体性能,本研究结果清楚地表明,欧文一致地发现模型和田中模型之一可以预测接近实验数据的混合模式疲劳寿命,而基于整体性能,理查德和阎的模型仍然是保守的模型,可以预测混合模式的疲劳寿命。模式疲劳寿命,这些结论已被发表的结果证实。

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