Finite element analysis of the behavior of bonded composite patches repair in aircraft structures

Finite element analysis of the behavior of bonded composite patches repair in aircraft structures

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This paper aims to analyze the multi-effects of the glass fiber reinforced polymer (GFRP) composite patch to repair the inclined cracked 2420-T3 aluminum plate. Three-dimensional finite element method (FEM) was used to study the effect of GFRP composite patch with different stacking composite lamin...

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Bibliographic Details
Main Authors: Islam El-Sagheer, Mai Taimour, Mariam Mobtasem, Amr Abd-Elhady, Hossam El-Din M. Sallam
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2020-09-01
Series:Frattura ed Integrità Strutturale
Subjects:
Mode of mixity
J-integral
Aluminum alloy
3-D FEM
Composite repair patch
Online Access:https://www.fracturae.com/index.php/fis/article/view/2863

Internet

https://www.fracturae.com/index.php/fis/article/view/2863

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