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

Show other versions (1)

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 lamina...

Full description

Bibliographic Details
Main Authors: I. El-Sagheer, M. Taimour, M. Mobtasem, Amr A. Abd-Elhady, Hossam El-Din M. Sallam
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2020-10-01
Series:Fracture and Structural Integrity
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/2863/3100

Internet

https://www.fracturae.com/index.php/fis/article/view/2863/3100

Similar Items