Fracture and Structural Integrity e-ISSN 1971-8993 Open access
Miscellanea Vol. 16, No. 60 (2022)

Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack

Author and affiliation details
  • Mohamed Berrahou Corresponding author University of Relizane, GIDD Laboratory, Relizane, Algeria mohamed.berrahou@univ-relizane.dz
  • Hayet Benzineb University of Relizane, GIDD Laboratory, Relizane, Algeria
  • Mohamed Serier University of Relizane, GIDD Laboratory, Relizane, Algeria
DOI
10.3221/IGF-ESIS.60.23
Pages
331-345
Published
Licence
CC BY 4.0
Published inVol. 16, No. 60 (2022)Go to the issue

Abstract

In this study, the finite element method is used to analyze the effect of corrosion and the behavior of inclined cracks of an aluminum plate Al 2024 -T3 under thermomechanical loading.  The effects of the inclination of the crack and the effect of temperature for and different types and shapes of adhesives are highlighted.  The results obtained show the increase of the crack inclination leads to a decrease of the damaged area and the damaged area ratio of the adhesive.  In addition, the ratio DR increases with increasing temperature variation ΔT.  The best performing patch shape that gave interesting results during this analysis is the circular and for type the Boron/epoxy is the best.

Keywords

Article history

  1. ReceivedUntil the next stage: 46 days
  2. RevisedUntil the next stage: 23 days
  3. AcceptedUntil the next stage: 32 days
  4. Published

How to cite

APA

Berrahou, M., Benzineb, H., & Serier, M. (2022). Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack. Fracture and Structural Integrity, 16(60), 331–345. https://doi.org/10.3221/IGF-ESIS.60.23

IEEE

M. Berrahou, H. Benzineb, and M. Serier, “Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack,” Fracture and Structural Integrity, vol. 16, no. 60, pp. 331–345, 2022, doi: 10.3221/IGF-ESIS.60.23.

MLA

Berrahou, Mohamed, et al. “Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack.” Fracture and Structural Integrity, vol. 16, no. 60, 2022, pp. 331–345. https://doi.org/10.3221/IGF-ESIS.60.23.

Chicago

Berrahou, Mohamed, Hayet Benzineb, and Mohamed Serier. 2022. “Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack.” Fracture and Structural Integrity 16 (60): 331–345. https://doi.org/10.3221/IGF-ESIS.60.23.

Harvard

Berrahou, M., Benzineb, H. and Serier, M. (2022) ‘Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack’, Fracture and Structural Integrity, 16(60), pp. 331–345. doi: 10.3221/IGF-ESIS.60.23.

Vancouver

Berrahou M, Benzineb H, Serier M. Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack. Fracture and Structural Integrity. 2022;16(60):331-345. doi:10.3221/IGF-ESIS.60.23

BibTeX

@article{berrahou2022, author = {Berrahou, Mohamed and Benzineb, Hayet and Serier, Mohamed}, title = {Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack}, journal = {Fracture and Structural Integrity}, year = {2022}, volume = {16}, number = {60}, pages = {331--345}, doi = {10.3221/IGF-ESIS.60.23}, url = {https://doi.org/10.3221/IGF-ESIS.60.23}, issn = {1971-8993} }

RIS

TY - JOUR AU - Berrahou, Mohamed AU - Benzineb, Hayet AU - Serier, Mohamed TI - Analysis of the adhesive damage for different shapes and types patch’s in Aircraft Structures corroded with an inclined crack JO - Fracture and Structural Integrity T2 - Fracture and Structural Integrity PY - 2022 DA - 2022/03/25 VL - 16 IS - 60 SP - 331 EP - 345 DO - 10.3221/IGF-ESIS.60.23 UR - https://doi.org/10.3221/IGF-ESIS.60.23 SN - 1971-8993 ER -

Licence

Creative Commons Attribution 4.0 International

May be shared and adapted, provided appropriate credit is given. Copyright © 2022 Mohamed Berrahou, Hayet Benzineb, Mohamed Serier.

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

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