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A novel formulation of the theory of critical distances to estimate lifetime of notched components in the medium-cycle fatigue regime

机译:临界距离理论的一种新公式,用于估计中周期疲劳状态下缺口构件的寿命

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In the present paper, the theory of critical distances (TCD) is reformulated in order to make it suitable for predicting fatigue lifetime of notched components in the medium-cycle fatigue regime. This extension of the TCD takes as its starting point the idea that the material characteristic length, L, changes as the number of cycles to failure, N_f, changes. In order to define the L versus N_f relationship two different strategies were investigated. Initially, we attempted to determine it by using the L values calculated considering material properties defined at the two extremes, namely static failure and the fatigue limit. This strategy, though correct from a philosophical point of view, contained some problems in its practical application. We subsequently attempted to determine the L versus N_f relationship by means of two calibration fatigue curves; (one generated by testing plain specimens and the second one generated by testing notched specimens). This second strategy was found to be much more simple to apply to practical problems, resulting in estimations characterized by a higher accuracy. The reliability of the devised method was systematically checked by using experimental results generated by testing notched specimens of low-carbon steel containing different geometrical features and tested using various loading types, stress ratios and specimen thicknesses. The accuracy of the method was further verified by using several data sets taken from the literature. Our method was seen to be successful giving predictions falling always within the scatter band of the data from the parent material. These results are very interesting, especially considering that the TCD is very easy to use because it requires only a linear-elastic stress analysis.
机译:在本文中,对临界距离(TCD)的理论进行了重新表述,以使其适合于预测中周期疲劳状态下缺口构件的疲劳寿命。 TCD的这种扩展以材料特征长度L随着失效循环数N_f的变化而变化的思想作为出发点。为了定义L与N_f的关系,研究了两种不同的策略。最初,我们尝试使用考虑到在两种极端情况下定义的材料特性(即静态破坏和疲劳极限)计算得出的L值来确定它。尽管从哲学的角度来看这种策略是正确的,但在其实际应用中仍存在一些问题。我们随后尝试通过两条校准疲劳曲线确定L与N_f的关系。 (一个通过测试普通样本生成,第二个通过测试缺口样本生成)。发现第二种策略适用于实际问题要简单得多,从而可以提高准确性。通过测试包含不同几何特征的低碳钢缺口试样并使用各种载荷类型,应力比和试样厚度进行测试的实验结果,系统地检验了该方法的可靠性。通过使用从文献中获得的几个数据集,进一步验证了该方法的准确性。我们的方法被证明是成功的,它提供的预测总是落在来自父材料的数据的分散带内。这些结果非常有趣,特别是考虑到TCD非常易于使用,因为它只需要进行线性弹性应力分析即可。

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