DBEM crack propagation in friction stir welded aluminum joints

被引:39
作者
Citarella, R. [1 ]
Carlone, P. [1 ]
Sepe, R. [2 ]
Lepore, M. [1 ]
机构
[1] Univ Salerno, Dept Ind Engn, Fisciano, SA, Italy
[2] Univ Naples Federico II, Dept Chem Mat & Prod Engn, Naples, Italy
关键词
Friction stir welding; Residual stress; DBEM multiple cracks growth; Contour method; Fatigue test; Butt joint; BOUNDARY-ELEMENT METHOD; BUTT JOINTS; GROWTH; PANEL; BEM;
D O I
10.1016/j.advengsoft.2015.12.002
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This paper deals with the simulation of multiple crack propagation in friction stir welded butt joints and the aim is to assess the influence of process induced residual stresses on the fatigue behavior of the assembly. The distribution of the process induced residual stresses is mapped by means of the contour method; then, the computed residual stress field is superimposed, in the DBEM environment, to the stress field due to a remote fatigue traction load and the crack growth is simulated. A two-parameters crack growth law is used for the crack propagation rate assessment. The Stress Intensity Factors are evaluated by the J-integral technique. Computational results have been compared with experimental data, provided by constant amplitude crack propagation tests on welded samples, showing the subdivision of the overall fatigue life in the two periods of crack initiation and crack propagation. (C) 2015 Civil-Comp Ltd. and Elsevier Ltd. All rights reserved.
引用
收藏
页码:50 / 59
页数:10
相关论文
共 23 条
[1]  
BUECKNER HF, 1958, T AM SOC MECH ENG, V80, P1225
[2]  
Carlone P, 2012, P 8 INT C ENG COMP T
[3]  
Carlone P., 2013, OPEN MECH ENG J, V7, P18, DOI DOI 10.2174/1874155X01307010018
[4]   A FEM-DBEM investigation of the influence of process parameters on crack growth in aluminum friction stir welded butt joints [J].
Carlone, Pierpaolo ;
Citarella, Roberto ;
Lepore, Marcello ;
Palazzo, Gaetano S. .
INTERNATIONAL JOURNAL OF MATERIAL FORMING, 2015, 8 (04) :591-599
[5]   Influence of Process Parameters on Microstructure and Mechanical Properties in AA2024-T3 Friction Stir Welding [J].
Carlone P. ;
Palazzo G.S. .
Metallography, Microstructure, and Analysis, 2013, 2 (4) :213-222
[6]   Three-Dimensional BEM and FEM Submodelling in a Cracked FML Full Scale Aeronautic Panel [J].
Citarella, R. ;
Cricri, G. .
APPLIED COMPOSITE MATERIALS, 2014, 21 (03) :557-577
[7]   Assessment of Crack Growth from a Cold Worked Hole by Coupled FEM-DBEM Approach [J].
Citarella, R. ;
Cricri, G. ;
Lepore, M. ;
Perrella, M. .
ADVANCES IN FRACTURE AND DAMAGE MECHANICS XII, 2014, 577-578 :669-672
[8]   Thermo-mechanical crack propagation in aircraft engine vane by coupled FEM-DBEM approach [J].
Citarella, R. ;
Cricri, G. ;
Lepore, M. ;
Perrella, M. .
ADVANCES IN ENGINEERING SOFTWARE, 2014, 67 :57-69
[9]   Multiple crack propagation with Dual Boundary Element Method in stiffened and reinforced full scale aeronautic panels [J].
Citarella, R. ;
Cricrì, G. ;
Armentani, E. .
Key Engineering Materials, 2013, 560 :129-155
[10]   A two-parameter model for crack growth simulation by combined FEM-DBEM approach [J].
Citarella, R. ;
Cricri, G. .
ADVANCES IN ENGINEERING SOFTWARE, 2009, 40 (05) :363-377