SIF for inclined cracks repaired with double and single composite patch

Mechanics of Advanced Materials and Structures

Volumn 14, Issue 4, 2007, Pages 303-308

  Bouiadjra, B Bachir ^a   Fekirini, H ^a   Serier, B ^a   Benguediab, M ^a  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

Author keywords

Adhesive stresses; Composite repair; Crack; Finite element method; Mixed mode; SIF

Indexed keywords

COMPOSITE MATERIALS; CRACKS; FINITE ELEMENT METHOD; PLATES (STRUCTURAL COMPONENTS); STRESS ANALYSIS;

ADHESIVE STRESSES; COMPOSITE REPAIR;

STRESS INTENSITY FACTORS;

EID: 34248562181     PISSN: 15376494     EISSN: 15376532     Source Type: Journal    
DOI: 10.1080/15376490600845454     Document Type: Article

References (17)

1. Baker, A. A., Callinan, R. J., Davis, M. J., Jones, R., and Williams, J. G., "Repair of mirage iii aircraft using BFRP crack patching technology," Theoritical and Applied Fracture Mechanics 2, 1-16 (1984).
2. Baker, A. A., "Repair of cracked or defective metallic components with advanced fibre composites: An overview of Australian work," Composite Structures 2, 153-81 (1984).
3. Baker, A. A., "On the certification of bonded composite repairs primary aircraft structures," Proceedings of the Eleventh International Conference of Composite Materials (ICCM-11), Gold Coast, Australia (1997).
4. Ting, T., Jones, R., Chiu, W. K., Marshall, I. H., and Greer, J. M., "Composites repairs to rib stiffened panels," Composite Structures 47, 737-743 (1999).
5. Callinan, R. J., Sanderson, S., and Keeley, D., "Finite element analysis of an F-111 lower wing skin fatigue crack repair," DSTO, Melbourne, DSTO-TN-0067 (1997).
6. Jones, R., and Chiu, W. K., "Composite repairs to crack in metallic components," Composite Structures 44 17-29 (1999).
7. Baker, A. A., "Joining and repair of aircraft composite structures," In: Mallick Pk (Ed.) Part 14, Composite Engineering Handbook, New York, Marcel Decker Inc., (1997).
8. Schubbe, J. J., and Mall, S., "Modeling of cracked thick metallic structure with bonded composite patch repair using three-layer technique," Composite Structures 45, 185-193 (1999).
9. Rose, L. R. F., "An application of the inclusion analogy for bonded reinforcements," International Journal of Solid and Structures 17, 827-38 (1981).
10. Bachir, B. B., Belhouari, M., and Serier, B., "Computation of the stress intensity factors for patched cracks with bonded composite repairs in mode I and mixed mode," Composite Structures 56, 401-406 (2002).
11. Megueni, A., Bachir, B. B., and Boutabout, B., "Computation of the Stress Intensity Factor for patched crack with bonded composite repair in pure Mode II," Composite Structure 59, 415-418 (2003).
12. Achour, T., Bachir, B. B., and Serier, B., "Numerical analysis of the performance of the bonded composite patch in reducing stress concentration and repairing crack at notch," Computational Material Sciences 28, 41-48 (2003).
13. Belhouari, M., Bachir Bouiadjra, B., and Serier, B., "Comparison of double and single bonded repairs to symmetric composite structures: A numerical analysis," Composite Structures 65, 47-53 (2004).
14. Turaga, V. R. S., and Ripudaman, S., "Modelling of patch repairs to a thin cracked sheet," Engineering Fracture Mechanics 62, 267-289 (1999).
15. Chen, W. H., and Yang, S. H., "Estimation of stress intensity factors in partially patched cracked composite laminates by multiplayer hybrid-stress finite element method," Finite Elements in Analysis and Design 21, 21-44 (1999).
16. Swenson, D., and James, M., FRANC2D/L: A crack propagation simulator for plane layered Structures. Version 1.4 User's guide (1998).
17. Henshel, R. D., and Shaw, K. G., "Crack tip finite elements are unnecessary," International Journal for Numerical Methods in Engineering 9, 495-507 (1975).