Thermal residual stresses effects on fatigue crack growth of repaired panels bounded with various composite materials
Author:
Publisher
Elsevier BV
Subject
Civil and Structural Engineering,Ceramics and Composites
Reference21 articles.
1. Bonded repair of aircraft structure;Baker,1988
2. Analysis of cracked aluminium plates repaired with bonded composite patches;Sun;AIAA J,1996
3. Successive 3D FE analysis technique for characterization of fatigue crack growth behaviour in composite-repaired aluminium plate;Lee;Comp Struct,2004
4. Experimental fatigue crack growth and crack-front shape analysis of asymmetric repaired aluminium panels with glass/epoxy composite patches;Hosseini-Toudeshky;Comp Struct,2005
5. Numerical and experimental fatigue crack growth analysis in mode-I for repaired aluminium panels using composite material;Hosseini-Toudeshky;Composites A,2007
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