Analysis of the adhesive damage for different patch shapes in bonded composite repair of aircraft structures-Reference-Cited by-同舟云学术

Analysis of the adhesive damage for different patch shapes in bonded composite repair of aircraft structures

Published:2014-02 Issue: Volume:54 Page:18-24
ISSN:0261-3069
Container-title:Materials & Design (1980-2015)
language:en
Short-container-title:Materials & Design (1980-2015)

Author:

Benyahia F.,Albedah A.,Bachir Bouiadjra B.

Publisher

Elsevier BV

Subject

Applied Mathematics,General Mathematics

Reference22 articles.

1. A proposed approach for certification of bonded composite repair to flight-critical airframe structure;Baker;Appl Compos Mater,2011

2. Analysis of cracked aluminum plates with one-sided patch repair using p-convergent layered model;Ahn;Finite Elem Anal Des,2010

3. Fatigue and residual strength performance of bonded repair to metallic fuselage;Bakuckas;Struct Integrity: Influence of Efficiency and Green Imperatives,2011

4. Optimization of a composite scarf repair patch under tensile loading;Breitzman;Compos Part A: Appl Sci Manuf,2009

5. Numerical analysis of the stress intensity factors for repaired cracks from a notch with bonded composite semicircular patch;Ouinas;Compos B Eng,2009

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