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

Composite Structures

Volumn 56, Issue 4, 2002, Pages 401-406

  Bachir Bouiadjra, B ^a   Belhouari, M ^a   Serier, B ^a  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

Author keywords

Bonded composite repairs; Crack; Finite element method; Patch; Stress intensity factor

Indexed keywords

ADHESIVES; CRACKS; FINITE ELEMENT METHOD; STRESS INTENSITY FACTORS;

COMPOSITE PATCHES;

COMPOSITE STRUCTURES;

AIRCRAFT; CRACKING; REPAIR; STRESS;

EID: 0036624128     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00023-5     Document Type: Article

References (15)

1. Repair of mirage iii aircraft using BFRP crack patching technology
2. Repair of cracked or defective metallic components with advanced fibre composites an overview of Australian work
3. Recent advances in bonded composite repair technology for metallic aircraft components
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5. On the certification of bonded composite repairs primary aircraft structures
6. Joining and repair of aircraft composite structures
7. Composites repairs to rib stiffened panels
8. Composite repairs to crack in metallic components
9. Modelling of patch repairs to a thin cracked sheet
10. Bonded composite repair for fatigue-cracked primary aircraft structure
11. FRANC2D/L: A crack propagation simulator for plane layered structures
12. Crack tip finite elements are unnecessary
13. An application of the inclusion analogy for bonded reinforcements