Numerical analysis for the determination of the stress intensity factors and crack opening displacements in plates repaired with single and double composite patches-Reference-Cited by-同舟云学术

Numerical analysis for the determination of the stress intensity factors and crack opening displacements in plates repaired with single and double composite patches

Published:2008-05 Issue:3 Volume:42 Page:385-393
ISSN:0927-0256
Container-title:Computational Materials Science
language:en
Short-container-title:Computational Materials Science

Author:

Madani K.,Touzain S.,Feaugas X.,Benguediab M.,Ratwani M.

Publisher

Elsevier BV

Subject

Computational Mathematics,General Physics and Astronomy,Mechanics of Materials,General Materials Science,General Chemistry,General Computer Science

Reference24 articles.

1. REPAIR EFFICIENCY IN FATIGUE-CRACKED ALUMINIUM COMPONENTS REINFORCED WITH BORON/EPOXY PATCHES

2. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch

3. Fatigue crack growth behavior of cracked aluminum plate repaired with composite patch

4. Bonded Repair of Aircraft Structures;Baker,1988

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