Modeling of a cracked and repaired Al 2024T3 aircraft plate: effect of the composite patch shape on the repair performance
In this work the finite element method was used to analyse the composite patch shape effect of the repair performance. Unlike all the works done conducted so far in this domain, this work proposed here, takes into account the reducing both, the stress intensity factor in repairing crack heads and th...
Saved in:
Main Authors: | Baghdadi Mohammed, Serier Boualem, Salem Mokadem, Zaoui Bouchra, Kaddouri Khacem |
---|---|
Format: | Article |
Language: | English |
Published: |
Gruppo Italiano Frattura
2019-10-01
|
Series: | Fracture and Structural Integrity |
Subjects: | |
Online Access: | https://www.fracturae.com/index.php/fis/article/view/2403/2688 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Modeling of a cracked and repaired Al 2024T3 aircraft plate: effect of the composite patch shape on the repair performance
by: Mohammed Baghdadi, et al.
Published: (2019-07-01) -
Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch
by: Nour Chafak Mohamed Ibrahim, et al.
Published: (2018-10-01) -
Finite element analysis of the thermomechanical behavior of metal matrix composites (MMC)
by: Zaoui Bouchra, et al.
Published: (2020-01-01) -
Study of mechanical behavior by fatigue of a cracked plate repaired by different composite patches
by: Moulgada Abdelmadjid, et al.
Published: (2021-04-01) -
Composite lay-up configuration effect on double and single sided bonded patch repairs
by: Toufik Achour, et al.
Published: (2022-07-01)