Stress concentration factors and fatigue behaviour of welded thin-walled CHS-SHS T-joints under in-plane bending

被引:69
作者
Mashiri, FR [1 ]
Zhao, XL [1 ]
Grundy, P [1 ]
机构
[1] Monash Univ, Dept Civil Engn, Clayton, Vic 3800, Australia
关键词
fatigue; hollow section join; stress concentration; hot spot stress; surface crack; through thickness crack;
D O I
10.1016/j.engstruct.2004.06.010
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Fatigue tests were carried out on welded thin-walled (t < 4 mm) T-joints made of circular hollow section (CHS) braces welded onto square hollow section (SHS) chords, under the loading conditions of "in-plane bending in the brace". Stress distributions were measured at different hot spot locations around the chord-brace junction, where cracks were observed to initiate and grow causing fatigue failure. The degree of non-linearity from the measured stress distributions around the weld toes of the brace-chord junction showed that stress distribution is significantly non-linear, along specified locations for brace diameter to chord width ratios greater than 0.5. The quadratic method of extrapolation of local strains/stresses to determine hot spot stresses is recommended. Using the measured stress distributions from this investigation and results from previous research, hot spot location lines that produce the highest hot spot stresses are recommended. The stress concentration factors (SCFs) for the welded thin-walled CHS-SHS T-joints lie in between the predicted values of SCFs for CHS-CHS and SHS-SHS T-joints for given non-dimensional parameters. A method is suggested for estimating SCFs for welded thin-walled CHS-SHS T-joints using existing parametric equations for SHS-SHS T-joints. An end of test failure criterion is chosen and shown to be a reliable method for obtaining fatigue data that can be used for producing design S-N curves. A through thickness crack is shown to occur when a surface crack has grown to a length equal to about 40% of the circumference of the weld toe in the chord. (C) 2004 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1861 / 1875
页数:15
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