Computation of the stress intensity factors for repaired cracks with bonded composite patch in mode I and mixed mode

Author:

Bachir Bouiadjra B,Belhouari M,Serier B

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference15 articles.

1. Repair of mirage iii aircraft using BFRP crack patching technology;Baker;Theor. Appl. Fracture Mech.,1984

2. Repair of cracked or defective metallic components with advanced fibre composites an overview of Australian work;Baker;Compos. Struct.,1984

3. Bonded repair of aircraft structures,1988

4. Recent advances in bonded composite repair technology for metallic aircraft components;Baker,1993

5. Baker AA. Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structure. Presented at FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures, Atlanta, 28–30 August 1996

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