Fracture and Structural Integrity e-ISSN 1971-8993 Open access
Structural Integrity and Durability of Structures Vol. 16, No. 62 (2022)

Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch

Author and affiliation details
  • Kouider Madani Corresponding author University of Djillali Liabes, Faculty of Technology, Sidi Bel Abbes, Algeria koumad10@yahoo.fr
  • Safaa Chahrazed Djebbar University of Djillali Liabes, LMSS Laboratory, Sidi Bel Abbes, Algeria
  • Nadia Kaddouri University of Djillali Liabes, Faculty of Technology, Sidi Bel Abbes, Algeria
  • Mohamed El Ajrami University of Djillali Liabes, LMSS Laboratory, Sidi Bel Abbes, Algeria
  • Mohamed Belhouari University of Djillali Liabes, Faculty of Technology, Sidi Bel Abbes, Algeria
DOI
10.3221/IGF-ESIS.62.22
Pages
304-325
Published
Licence
CC BY 4.0

Abstract

The presence of a geometric discontinuity such as a crack or a notch can cause the failure of a structure during its use. Under various mechanical or thermal stresses, a high concentration of stresses can take place at the level of these discontinuities, which in most cases will lead to the total failure of the structure. The service life of these structures can be improved with the use of the repair technique by bonding a composite patch. This technique is of significant interest in several fields, especially with the use of composite materials. This technique is widely used in aeronautics and ensures a long life of damaged structures. Current research aims to optimize the shape size and fiber's nature of this composite patch in order to ensure good load transfer by reducing the stresses in the damaged area. In this work, a finite element method is used to analysis the effect of the shape of the patch on the global response of a 2024-T3 aluminum structure in the presence of a central circular notch. The composite patch is of the carbon/epoxy type bonded through an A-140 Adekit type adhesive on the damaged part of the plate. The analysis consists in determining the force-displacement curves of the repaired structure by using the combination of the two techniques, XFEM for the damage of the aluminum plate 2024-T3 by the automatic creation of the crack and CZM for the analysis of the adhesive debonding. The analysis takes into account the damage in the plate and in the adhesive. However, for the composite patch, and since there will be no damage, we have just analyzed the effect of its shape and essentially the shape of its edges on the load transfer and consequently on the resistance of the structure under loading in tension. Two main patch shapes have been highlighted, namely the square and circular shape. The results show clearly that the shape of the patch’s edges has an impact on the stresses reduction in the plate and subsequently ensures good resistance in terms of force-displacement curve and consequently delays the peeling of the adhesive.

Keywords

Article history

  1. ReceivedUntil the next stage: 60 days
  2. Revision requestedUntil the next stage: 24 days
  3. RevisedUntil the next stage: 41 days
  4. AcceptedUntil the next stage: 41 days
  5. Published

Statements

Funding

no supporting agencies

How to cite

APA

Madani, K., Djebbar, S. C., Kaddouri, N., El Ajrami, M., & Belhouari, M. (2022). Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch. Fracture and Structural Integrity, 16(62), 304–325. https://doi.org/10.3221/IGF-ESIS.62.22

IEEE

K. Madani, S. C. Djebbar, N. Kaddouri, M. El Ajrami, and M. Belhouari, “Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch,” Fracture and Structural Integrity, vol. 16, no. 62, pp. 304–325, 2022, doi: 10.3221/IGF-ESIS.62.22.

MLA

Madani, Kouider, et al. “Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch.” Fracture and Structural Integrity, vol. 16, no. 62, 2022, pp. 304–325. https://doi.org/10.3221/IGF-ESIS.62.22.

Chicago

Madani, Kouider, Safaa Chahrazed Djebbar, Nadia Kaddouri, Mohamed El Ajrami, and Mohamed Belhouari. 2022. “Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch.” Fracture and Structural Integrity 16 (62): 304–325. https://doi.org/10.3221/IGF-ESIS.62.22.

Harvard

Madani, K., Djebbar, S.C., Kaddouri, N., El Ajrami, M. and Belhouari, M. (2022) ‘Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch’, Fracture and Structural Integrity, 16(62), pp. 304–325. doi: 10.3221/IGF-ESIS.62.22.

Vancouver

Madani K, Djebbar SC, Kaddouri N, El Ajrami M, Belhouari M. Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch. Fracture and Structural Integrity. 2022;16(62):304-325. doi:10.3221/IGF-ESIS.62.22

BibTeX

@article{madani2022, author = {Madani, Kouider and Djebbar, Safaa Chahrazed and Kaddouri, Nadia and El Ajrami, Mohamed and Belhouari, Mohamed}, title = {Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch}, journal = {Fracture and Structural Integrity}, year = {2022}, volume = {16}, number = {62}, pages = {304--325}, doi = {10.3221/IGF-ESIS.62.22}, url = {https://doi.org/10.3221/IGF-ESIS.62.22}, issn = {1971-8993} }

RIS

TY - JOUR AU - Madani, Kouider AU - Djebbar, Safaa Chahrazed AU - Kaddouri, Nadia AU - El Ajrami, Mohamed AU - Belhouari, Mohamed TI - Use of combined CZM and XFEM techniques for the patch shape performance analysis on the behavior of a 2024-T3 aluminum structure reinforced with a composite patch JO - Fracture and Structural Integrity T2 - Fracture and Structural Integrity PY - 2022 DA - 2022/09/22 VL - 16 IS - 62 SP - 304 EP - 325 DO - 10.3221/IGF-ESIS.62.22 UR - https://doi.org/10.3221/IGF-ESIS.62.22 SN - 1971-8993 ER -

Licence

Creative Commons Attribution 4.0 International

May be shared and adapted, provided appropriate credit is given. Copyright © 2022 Kouider Madani, Safaa Chahrazed Djebbar, Nadia Kaddouri, Mohamed El Ajrami, Mohamed Belhouari.

Copyright 
Authors are allowed to retain both the copyright and the publishing rights of their articles without restrictions.  

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