A study on the fatigue crack growth behavior of thick aluminum panels repaired with a composite patch

Author:

Chung Ki-Hyun,Yang Won-Ho

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference17 articles.

1. Rastogi N, Soni SR, Denny JJ. Analysis of bonded composite patch repaired metallic structures: an overview. AIAA-98-1983, 1998. p. 1578–88

2. Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches;Baker;Fatigue Fract. Eng. Mater. Struct.,1993

3. Bonded repair of aircraft structure;Baker,1988

4. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch;Denney;Eng. Fract. Mech.,1997

5. Fredell R, Barneveld WV, Volt A. Analysis of composite patching of fuselage structures: high patch elastic modulus isn’t the whole story. In: Proceedings of the 39th International SAMPE Symposium, Anaheim, CA, April 11–14, 1994. p. 610–23

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