3-D modelling of cyclically loaded composite patch repair of a cracked plate-Reference-Cited by-同舟云学术

3-D modelling of cyclically loaded composite patch repair of a cracked plate

Published:2007-06 Issue:4 Volume:78 Page:486-494
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Ellyin Fernand,Ozah Folarin,Xia Zihui

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference32 articles.

1. Avram JB. Fatigue response of thin stiffened aluminum cracked panels repaired with bonded composite patches. AFIT/GMS/ENY/01M-01, School of Engineering, Air Force Institute of Technology (AU), Wright-Patterson AFB OH, 2001.

2. Investigation of the size effect of composite patching repaired on edge-cracked plates;Wang;Compos Struct,2000

3. Fatigue crack growth behavior of cracked aluminum plate repaired with composite patch;Seo;Compos Struct,2002

4. A study on the fatigue crack growth behaviour of thick aluminum panels repaired with a composite patch;Chung;Compos Struct,2003

5. Bonded composite repair for fatigue-cracked primary aircraft structure;Baker;Compos Struct,1999

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