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首页> 外文期刊>Journal of engineering materials and technology >An Elasto-Plastic Reformulation of the Theory of Critical Distances to Estimate Lifetime of Notched Components Failing in the Low/Medium-Cycle Fatigue Regime
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An Elasto-Plastic Reformulation of the Theory of Critical Distances to Estimate Lifetime of Notched Components Failing in the Low/Medium-Cycle Fatigue Regime

机译:临界距离理论的弹塑性重构,以估计低/中周期疲劳状态下缺口构件的寿命

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摘要

This paper is concerned with a novel elasto-plastic reformulation of the Theory of Critical Distances (TCD) specifically devised to estimate lifetime of notched metallic materials (ferrous and nonferrous) failing in the low/medium-cycle fatigue regime. We used the classic Manson-Coffin and Smith-Topper-Watson approaches, but applied in conjunction with the TCD. We assumed that the material's critical distance is a constant whose value does not depend on either the sharpness of the notch or on the number of cycles to failure. The accuracy and reliability of the proposed approach was checked by using a number of experimental results generated by testing cylindrical specimens made of En3B, which is a commercial low-carbon steel, and Al6082, which is a conventional aluminum alloy, containing different geometrical features and tested at applied load ratios of R = -1 and R=0. The resulting predictions of fatigue life were highly accurate, giving estimates falling within an error factor (in lifetime) of about 2. This result is undoubtedly encouraging, especially in light of the fact that the pieces of experimental information needed to calibrate our method can easily be generated by using standard testing equipment, and the necessary stress/strain fields acting on the fatigue process zone can be determined by directly postprocessing elasto-plastic finite element results.
机译:本文关注临界距离理论(TCD)的新颖弹塑性改写,该理论专门设计用于估计在低/中周期疲劳状态下失效的缺口金属材料(铁和非铁)的寿命。我们使用了经典的Manson-Coffin和Smith-Topper-Watson方法,但与TCD结合使用。我们假设材料的临界距离是一个常数,其值既不取决于切口的清晰度,也不取决于失效循环的次数。该方法的准确性和可靠性是通过使用大量的实验结果来检验的,这些结果是通过测试圆柱形样品(由商用低碳钢En3B和常规铝合金Al6082)制成的,该圆柱形样品包含不同的几何特征,并且在施加的负载比R = -1和R = 0时进行了测试。由此产生的疲劳寿命预测是非常准确的,给出的估计值落入约2的误差因子之内。这一结果无疑是令人鼓舞的,尤其是考虑到校准我们的方法所需的实验信息很容易通过使用标准的测试设备可以产生应力,并且可以通过直接对弹塑性有限元结果进行后处理来确定作用在疲劳过程区域上的必要应力/应变场。

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