表面缺口与次表面孔洞相互作用的应力集中因子

Q4 Engineering
Silas Z. Gebrehiwot, H. Remes, Anssi T. Karttunen
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引用次数: 1

摘要

我们提出了一种保守的方法来计算相互作用的缺口-孔对和双半圆缺口(即在其尖端前面有一个额外的小半圆缺口)的最大应力集中系数(SCF)。该方法基于圆孔的线性弹性Airy应力函数解。缺口孔和双缺口结构相对于均匀的单轴(水平)应力垂直对齐。这意味着,一个均匀的水平张力被应用到一个缺口孔对,躺在垂直轴上。对于缺口-孔对,计算了孔径分别为2.5a、5a、10a和15a时的最大相互作用scf,其中a为孔半径。通过二维有限元计算验证了分析结果。与详细的有限元分析相比,所提出的简单方法在大多数情况下提供了良好的结果,误差远低于10%。在疲劳分析中,确定了可被视为有效scf的疲劳缺口因子。通过使用简单的方法,可以避免计算成本高昂的有限元分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Stress concentration factor for interacting surface notch and subsurface hole
We propose a conservative method for the calculation of the maximum stress concentration factor (SCF) for an interacting notch-hole pair and for a double semi-circular notch (i.e., a notch that has an additional small semi-circular notch ahead of its tip). The method is based on a linearly elastic Airy stress function solution for a circular hole. The notch-hole and double notch configurations are aligned vertically with respect to uniform uniaxial (horizontal) stress. This means, a uniform horizontal tension is applied to a notch-hole pair that lie on a vertical axis. For the notch-hole pair, the maximum interacting SCFs are calculated for edge to edge gaps equal to hole sizes of 2.5a, 5a, 10a and 15a, where a is the hole radius. The analytical results are validated by 2-D finite element calculations. The presented simple approach provides good results with errors well below 10% in most cases compared to the detailed finite element analyses. Fatigue notch factors that can be thought of as the effective SCFs in fatigue analyses are determined. By using the simple approach, computationally costly finite element analysis can be avoided.
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来源期刊
Rakenteiden Mekaniikka
Rakenteiden Mekaniikka Engineering-Mechanical Engineering
CiteScore
0.50
自引率
0.00%
发文量
2
审稿时长
16 weeks
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