Analysis of load-displacement curves of an adhesive-reinforced composite patch repaired plate using the combination of XFEM and CZM techniques

被引:7
作者
Benyettou, M. [1 ]
Madani, K. [1 ]
Djebbar, S. C. [1 ]
Amin, H. [2 ]
Belhouari, M. [1 ]
Elajrami, M. [1 ]
Feaugas, X. [3 ]
Campilho, R. D. S. G. [4 ,5 ]
机构
[1] Univ Djillali Liabes Sidi Bel Abbes, Dept Mech Engn, BP 89,Cite Ben Mhidi, Sidi Bel Abbes 22000, Algeria
[2] Univ MHamed Bougara Boumerdes, Fac Technol, Mech Engn Dept, Boumerdes, Algeria
[3] Univ La Rochelle, LaSIE, Lab Sci Ingn Environm, UMR7356, La Rochelle, France
[4] Polytech Porto, Sch Engn, CIDEM, ISEP, R Dr Antonio Bernardino Almeida,431, P-4200072 Porto, Portugal
[5] INEGI Polo FEUP, Rua Dr Roberto Frias,400, P-4200465 Porto, Portugal
关键词
XFEM; CZM; Repaired plate; Adhesive; Crack; FATIGUE-CRACK GROWTH; STRESS INTENSITY FACTORS; NUMERICAL-ANALYSIS; TENSILE BEHAVIOR; ALUMINUM PLATE; FRACTURE; PREDICTION; SINGLE; JOINTS; DAMAGE;
D O I
10.1016/j.ijadhadh.2024.103885
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
Since the development of the eXtended Finite Element Method (XFEM), Cohesive Zone Modelling (CZM), and the Virtual Crack Closure Technique (VCCT) for damage analysis in repaired structures, it has now become easy to validate experimental tensile tests carried out on damaged and repaired plates with a composite patch. In most cases, these tensile tests can be expensive and time-consuming due to surface preparation, cleaning, polishing, adhesive application, and the crosslinking time of the adhesive, which must be carefully considered. The analysis of damage in structures assembled by adhesive bonding is crucial to predicting their behavior under various loading conditions. Moreover, the analysis of experimental curves is in most cases translated a global behavior without taking into account the details that can influence the results. With the introduction of techniques (XFEM, CZM and VCCT), it is now possible to model different forms of damage, accounting for several mechanical and geometric parameters of the plate, patch, and adhesive. This work aims to analyze the behavior under tensile loading of a 2024-T3 aluminum plate presenting an initial crack of different lengths emanating from a central circular notch. This plate is repaired by a carbon/epoxy type patch through an adekit A140 adhesive. The combined use of XFEM to track damage in the plate and CZM for adhesive debonding allowed the acquisition of tensile load-elongation curves and the assessment of damage inflicted by loading on the plate. The results demonstrate that the combined use of XFEM and CZM techniques enables the identification of the adhesive debonding impact on the load transfer to the patch and consequently on the strength of the repaired structure. Furthermore, these highlight that the decrease in the effectiveness of the composite patch with increasing crack size is directly linked to the progressive deterioration of both the plate and the adhesive strength.
引用
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页数:14
相关论文
共 55 条
[41]   Numerical investigation of composite patch repair of inclined cracked panel using XFEM [J].
Makwana, Alpesh H. ;
Vyas, Nisarg ;
Barot, R. S. .
MATERIALS TODAY-PROCEEDINGS, 2021, 45 :5128-5133
[42]   Investigation of patch hybridization effect on the composite patch repair of a cracked aluminum plate: A pragmatic approach [J].
Makwana, Alpesh H. ;
Shaikh, A. A. ;
Bakare, A. K. ;
Chitturi, Saikrishna .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2019, 26 (17) :1458-1468
[43]   Modelling Damage and Failure in Adhesive Joints Using A Combined XFEM-Cohesive Element Methodology [J].
Mubashar, A. ;
Ashcroft, I. A. ;
Crocombe, A. D. .
JOURNAL OF ADHESION, 2014, 90 (08) :682-697
[44]   Analysis of the presence of bonding defects on the fracture behavior of a damaged plate repaired by composite patch [J].
Nadia, Kaddouri ;
Madani, Kouider ;
Bellali, Mohammed Amine ;
Feaugas, Xavier .
FRATTURA ED INTEGRITA STRUTTURALE, 2019, 49 (49) :331-340
[45]   Fracture properties of epoxy asphalt mixture based on extended finite element method [J].
Qian Zhen-dong ;
Hu Jing .
JOURNAL OF CENTRAL SOUTH UNIVERSITY, 2012, 19 (11) :3335-3341
[46]   Influence of water ingress onto the crack propagation rate in a AA2024-T3 plate repaired by a carbon/epoxy patch [J].
Rezgani, L. ;
Madani, K. ;
Feaugas, X. ;
Touzain, S. ;
Cohendoz, S. ;
Valette, J. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 55 :359-365
[47]  
Schubbe JJ, 2016, Fatigue crack growth behavior of aerospace and ship-grade aluminum repaired with composite patches in a corrosive environment
[48]   Fatigue crack growth behavior of cracked aluminum plate repaired with composite patch [J].
Seo, DC ;
Lee, JJ .
COMPOSITE STRUCTURES, 2002, 57 (1-4) :323-330
[49]   FAILURE PREDICTION TECHNIQUE FOR COMPRESSION LOADED CARBON FIBER-EPOXY LAMINATE WITH OPEN HOLES [J].
SOUTIS, C ;
FLECK, NA ;
SMITH, PA .
JOURNAL OF COMPOSITE MATERIALS, 1991, 25 (11) :1476-1498
[50]   Compressive behaviour of CFRP laminates repaired with adhesively bonded external patches [J].
Soutis, C ;
Duan, DM ;
Goutas, P .
COMPOSITE STRUCTURES, 1999, 45 (04) :289-301