Evaluating stress intensity factors due to weld residual stresses by the weight function and finite element methods

被引:71
作者
Bao, Rui [2 ]
Zhang, Xiang [1 ]
Yahaya, Norvahida Ahmad [1 ]
机构
[1] Cranfield Univ, Sch Engn, Dept Aerosp Engn, Cranfield MK43 0AL, Beds, England
[2] Beihang Univ, Sch Aeronaut Sci & Engn, Inst Solid Mech, Beijing 100191, Peoples R China
关键词
Welded joints; Residual stresses; Stress intensity factor; Finite element analysis; Weight function; FATIGUE-CRACK-GROWTH; FIELD; PROPAGATION; COMPUTATION; 2024-T351; BEHAVIOR; STRIP;
D O I
10.1016/j.engfracmech.2010.06.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper presents a study on the application of the weight function and finite element methods to evaluate residual stress intensity factors in welded test samples. Three specimen geometries and various residual stress profiles were studied. Comparisons of the two different methods were made in terms of the accuracy, easiness to use, conditions and limitations. Calculated residual stress intensity factors by the two different methods are in general in good agreement for all the configurations studied. Computational issues involved in executing these methods are discussed. Some practical issues are also addressed, e.g. treatment of incomplete or limited residual stress measurements, influence of transverse residual stresses, and modelling residual stress in short-length specimens. The finite element method is validated by well-established weight functions and thus can be applied to complex geometries following the procedures recommended in this paper. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2550 / 2566
页数:17
相关论文
共 34 条
[1]  
[Anonymous], 2005, FRACTURE MECH FUNDAM
[2]   A general weight function for inclined cracks at sharp V-notches [J].
Beghini, M. ;
Bertini, L. ;
Di Lello, R. ;
Fontanari, V. .
ENGINEERING FRACTURE MECHANICS, 2007, 74 (04) :602-611
[3]   Stress intensity factors for an inclined edge crack in semiplane [J].
Beghini, M ;
Bertini, L ;
Fontanari, V .
ENGINEERING FRACTURE MECHANICS, 1999, 62 (06) :607-613
[4]   FATIGUE-CRACK GROWTH IN RESIDUAL-STRESS FIELDS - EXPERIMENTAL RESULTS AND MODELING [J].
BEGHINI, M ;
BERTINI, L ;
VITALE, E .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 1994, 17 (12) :1433-1444
[5]   FATIGUE CRACK-PROPAGATION THROUGH RESIDUAL-STRESS FIELDS WITH CLOSURE PHENOMENA [J].
BEGHINI, M ;
BERTINI, L .
ENGINEERING FRACTURE MECHANICS, 1990, 36 (03) :379-387
[6]  
BUECKNER HF, 1970, Z ANGEW MATH MECH, V50, P529
[7]  
Elber W., 1971, Damage tolerance in aircraft structures, P230, DOI DOI 10.1520/STP486-EB
[8]   ON THE CALCULATION OF CRACK OPENING DISPLACEMENT FROM THE STRESS INTENSITY FACTOR [J].
FETT, T ;
MATTHECK, C ;
MUNZ, D .
ENGINEERING FRACTURE MECHANICS, 1987, 27 (06) :697-715
[9]   APPROXIMATE WEIGHT FUNCTION FOR 2D AND 3D-PROBLEMS [J].
FETT, T ;
MATTHECK, C ;
MUNZ, D .
ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS, 1989, 6 (01) :48-63
[10]   Fatigue crack growth in 2024-T351 friction stir welded joints: Longitudinal residual stress and microstructural effects [J].
Fratini, L. ;
Pasta, S. ;
Reynolds, A. P. .
INTERNATIONAL JOURNAL OF FATIGUE, 2009, 31 (03) :495-500