Fracture energy for repaired cracks with bonded composite patch having two adhesive bands in aircraft structures

Computational Materials Science

Volumn 40, Issue 1, 2007, Pages 20-26

  Bachir Bouiadjra, B ^a   Fekirini, H ^a   Belhouari, M ^a   Boutabout, B ^a   Serier, B ^a  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

Author keywords

Adhesive stress; Bonded composite repair; Crack; Energy release rate; Finite element method; Two adhesive band

Indexed keywords

ADHESIVE JOINTS; AIRCRAFT PARTS AND EQUIPMENT; ENERGY RELEASE RATE; FINITE ELEMENT METHOD; FRACTURE ENERGY; STRESS ANALYSIS;

ADHESIVE STRESS; ALUMINIUM COMPONENT; BONDED COMPOSITE REPAIR; TWO ADHESIVE BAND;

CRACK DETECTION;

EID: 34248203706     PISSN: 09270256     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.commatsci.2006.10.016     Document Type: Article

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