Numerical and experimental fatigue crack growth analysis in mode-I for repaired aluminum panels using composite material
Author:
Publisher
Elsevier BV
Subject
Mechanics of Materials,Ceramics and Composites
Reference14 articles.
1. Bonded repair of aircraft structures;Baker,1988
2. Crack patching;Baker,1988
3. Fatigue crack growth behaviour of cracked aluminum plate repaired with composite patch;Seo;Compos Struct,2002
4. Analysis of cracked adhesively bonded laminated structures;Ratwani;AIAA J,1979
5. A cracked plate repaired by bonded reinforcements;Rose;Int J Fract,1982
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