An enhanced stress field intensity approach for fatigue life assessment combining notch and size effect

被引:5
作者
Wang, Zinan [1 ]
Kong, Xiangwei [1 ,2 ,3 ]
Xie, Liyang [1 ,2 ,3 ]
Wu, Ningxiang [1 ,2 ,3 ]
Zhen, Cheng [1 ]
Gu, Jianyi [1 ]
机构
[1] Northeastern Univ, Sch Mech Engn & Automat, Shenyang 110819, Peoples R China
[2] Northeastern Univ, Key Lab Vibrat & Control Aeroprop Syst, Minist Educ, Shenyang 110819, Peoples R China
[3] Northeastern Univ, Liaoning Prov Key Lab Multidisciplinary Design Opt, Shenyang 110819, Peoples R China
关键词
Notch effect; Stress field intensity approach; Size effect; Relative stress gradient; Fatigue life prediction; LOW-CYCLE FATIGUE; CRACK INITIATION; MULTIAXIAL FATIGUE; CRITICAL DISTANCE; PREDICTION; COMPONENTS; MODEL; STEEL; LIMIT; FORMULATION;
D O I
10.1016/j.ijfatigue.2024.108239
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The notch characteristics of engineering components significantly impact their fatigue lives. Accurately analyzing the notch effect and size effect is of great significance for structural integrity evaluation, which provides insights into the extent of fatigue failure in engineering structures. In this paper, a new method is proposed for determining the fatigue failure region based on actual elastic-plastic stress distribution under various notch geometries and applied loads. It considers the complex mechanical behavior of the plastic effect and stress relaxation near the notch root. Furthermore, a novel weight function is employed to consider the relative stress gradient at all points within the fatigue failure region. Finally, an enhanced stress field intensity approach is developed to predict notch specimens fatigue lives utilizing experimental lives of smooth specimens. Additionally, the effectiveness of the proposed method is analyzed by predicting the fatigue lives of three distinct materials notched specimens with varying geometries and applied loads. The prediction absolute errors of the proposed approach are compared with those of the other traditional notched fatigue analysis methods. The comparative results indicated that the performance of the proposed method outperforms the other methods.
引用
收藏
页数:16
相关论文
共 81 条
[1]   Fatigue behaviour of AlMgSi tubular specimens subjected to bending-torsion loading [J].
Abreu, L. M. P. ;
Costa, J. D. ;
Ferreira, J. A. M. .
INTERNATIONAL JOURNAL OF FATIGUE, 2009, 31 (8-9) :1327-1336
[2]   HCF of AA7050 alloy containing surface defects: Study of the statistical size effect [J].
Abroug, Foued ;
Pessard, Etienne ;
Germain, Guenael ;
Morel, Franck .
INTERNATIONAL JOURNAL OF FATIGUE, 2018, 110 :81-94
[3]   Fatigue life duration prediction for welded spots by volumetric method [J].
Adib, H ;
Gilgert, J ;
Pluvinage, G .
INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (01) :81-94
[4]   Theoretical and numerical aspects of the volumetric approach for fatigue life prediction in notched components [J].
Adib, H ;
Pluvinage, G .
INTERNATIONAL JOURNAL OF FATIGUE, 2003, 25 (01) :67-76
[5]   Advanced volumetric method for fatigue life prediction using stress gradient effects at notch roots [J].
Adib-Ramezani, H. ;
Jeong, J. .
COMPUTATIONAL MATERIALS SCIENCE, 2007, 39 (03) :649-663
[6]   Probabilistic modeling of fatigue life distribution and size effect of components with random defects [J].
Ai, Y. ;
Zhu, S. P. ;
Liao, D. ;
Correia, J. A. F. O. ;
Souto, C. ;
De Jesus, A. M. P. ;
Keshtegar, B. .
INTERNATIONAL JOURNAL OF FATIGUE, 2019, 126 :165-173
[7]   Stress gradient effect on crack initiation in fretting using a multiaxial fatigue framework [J].
Amargier, R. ;
Fouvry, S. ;
Chambon, L. ;
Schwob, C. ;
Poupon, C. .
INTERNATIONAL JOURNAL OF FATIGUE, 2010, 32 (12) :1904-1912
[8]  
[Anonymous], 2002, China Aeronautical Materials Handbook
[9]  
[Anonymous], 2004, Fracture and Fatigue Emanating from Stress Concentrators, DOI [10.1007/1-4020-2612-9, DOI 10.1007/1-4020-2612-9]
[10]  
Bailon J-P, Fatigue Mechanisms: Advances in Quantitative Measurement of Physical Damage, P313, DOI [10.1520/STP30563S, DOI 10.1520/STP30563S]