计算 20 千赫疲劳裂纹增长测试的应力强度因子范围

IF 1.8 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Mohamed Sadek, Jens Bergström, Nils Hallbäck
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引用次数: 0

摘要

惯性和阻尼会影响高频加载时的应力强度因子(SIF)值,因此必须将其纳入计算。在本研究中,针对两种类型的试样几何形状采用了不同的动态模拟程序,并对获得的 SIF 值进行了比较。谐波模态分析和直接稳态分析等快速计算程序与计算成本高昂的瞬态动态分析进行了比较。应用并比较了两种不同的 SIF 计算方法,即 J 积分法和裂纹尖端张开位移法(CTOD),结果表明在计算模态 I SIF 时几乎完全一致。在动态计算中引入了瑞利阻尼模型,以研究其影响,结果显示在 20 kHz 频率下对 SIF 有明显影响。在使用不同阻尼值的情况下,快速直接稳态分析与谐波模态分析和瞬态分析都显示出很好的一致性,因此在这项研究之后,推荐使用这种方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Computing the stress intensity factor range for fatigue crack growth testing at 20 kHz

Computing the stress intensity factor range for fatigue crack growth testing at 20 kHz

Inertia and damping influence the values of the stress intensity factors (SIFs) at high-frequency loading and they must be included in computations. In the present study, different dynamic simulation procedures were carried out for two types of specimen geometries and the achieved SIF values were compared. Fast computation procedures such as harmonic modal analysis and direct steady-state analysis were compared to the computationally expensive transient dynamic analysis. Two different methods for calculating the SIF, the J-integral and the crack tip opening displacement (CTOD) methods, were applied and compared and the results showed a near perfect agreement in calculation of the mode I SIF. The Rayleigh damping model was introduced into the dynamic computation to investigate its effect and the results revealed a clear effect on the SIF at 20 kHz frequency. The fast direct steady-state analysis showed good agreement to both harmonic modal and transient analysis with the different damping values used and is, after this study, the recommended procedure.

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CiteScore
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