Linear coupled bending and extension of an unbalanced bonded repair

International Journal of Solids and Structures

Volumn 44, Issue 10, 2007, Pages 3156-3176

  Clark, R J ^a   Romilly, D P ^a  

^a UNIVERSITY OF BRITISH COLUMBIA   (Canada)

Author keywords

Bending; Bonded repair; Coupling; Damage tolerance; Fatigue; Fracture; Line spring

Indexed keywords

BENDING (DEFORMATION); CRACK TIPS; DAMAGE TOLERANCE; FATIGUE OF MATERIALS; FRACTURE; INTERPOLATION; MATHEMATICAL MODELS; MAXWELL EQUATIONS; REPAIR; SHEAR STRESS;

BONDED COMPOSITE REPAIR DESIGNS; CLOSED FORM EQUATIONS; LINE SPRING; MAXWELL'S RECIPROCAL THEOREM;

COMPOSITE MATERIALS;

EID: 33947143711     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijsolstr.2006.09.012     Document Type: Article

References (31)

1. Albat A.M., and Romilly D.P. A direct linear-elastic analysis of double-symmetric bonded joints and reinforcements. Composites Science and Technology 59 (1999) 1127-1137
2. ANSYS Release 9.0., 2004. ANSYS Inc. Canonsburg, Pennsylvania, USA.
3. Arendt, C., Sun, C.T., 1994. Bending effects of asymmetric adhesively bonded composite repairs on cracked aluminum panels. In: Proceedings of the FAA/NASA International Symposium on Advanced Structural integrity for Airframe Durability and Damage Tolerance, NASA conference publication 3274, Part1, pp. 33-48.
4. Baker A.A. Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches. Fatigue and Fracture of Engineering Materials and Structures 16 7 (1993) 753-765
5. Clark R.J., and Romilly D.P. Fatigue damage prediction for bonded composite repairs applied to metallic aircraft structures. SAE Journal of Aerospace (2001) paper# 2001-01-26
6. Clark, R.J., Romilly, D.P., 2002. Experimental study of a bonded composite repair. 2002 CSME Forum, May 21-24, Kingston, Ontario, Canada.
7. Clark R.J., Romilly D.P., 2003. Non-linear bending study of hybrid aluminum and boron-epoxy bonded joints. CANCOM 2003, Ottawa, Ontario, Canada.
8. Clark, R.J., Romilly, D.P., submitted for publication. Reinforced cracks in transversally isotropic generalized pane strain plates. Theoretical and Applied Fracture Mechanics.
9. Clark R.J., Romilly D.P., submitted for publication. Bending of transversally isotropic generalized plane strain plates with reinforced cracks. International Journal of Fracture.
10. Duong C.N., and Wang C.H. On the characterization of fatigue crack growth in a plate with a single-sided repair. Transactions of the ASME 126 (2004) 192-198
11. Goland M., and Reissner E. The stresses in cemented joints. Journal of Applied Mechanics - Transactions of the ASME 66 (1949) A17-A27
12. Jones R. Neutral axis offset effects due to crack patching. Composite Structures 1 (1983) 163-174
13. Jones R., Callinan R.J., and Aggarwal K.C. Analysis of bonded repairs to damaged fibre composite structures. Engineering Fracture Mechanics 17 1 (1983) 37-46
14. Jones R., Chiu W.K., and Smith R. Airworthiness of composite repairs: failure mechanisms. Engineering Failure Analysis 2 2 (1995) 117-128
15. Joseph, P.F., Erdogan, F., 1987. Plates and shells containing a surface crack under general loading conditions. NASA contractor report 178232, NASA Langley Research Center.
16. Joseph P.F., and Erdogan F. Surface crack problems in plates. International Journal of Fracture 41 (1989) 105-131
17. Kotousov A., and Wang C.H. Fundamental solutions for the generalized plane strain theory. International Journal of Engineering Science 40 (2002) 1775-1790
18. Papanikos P., Tserpes K.I., Labeas G., and Pantelakis Sp. Progressive damage modelling of bonded composite repairs. Theoretical and Applied Fracture Mechanics 43 (2005) 189-198
19. Ratwani M.M. Cracked adhesively bonded laminated structures. AIAA Journal 17 9 (1979) 988-994
20. Romilly D.P., Clark R.J., 2005. Damage tolerance analysis and testing of unbalanced bonded composite repairs for aluminum airframes. SAE 05-AMT-41.
21. Rose L.R.F. An application of the inclusion analogy for bonded reinforcements. International Journal of Solids and Structures 17 (1981) 827-838
22. Rose L.R.F. A cracked plate repaired by bonded reinforcements. International Journal of Fracture 18 2 (1982) 135-144
23. Rose, L.R.F., 1988. Theoretical Analysis of crack patching. In: Baker, A.A., Jones, R., (eds.), Bonded Repair of Aircraft Structures. Martinus Nijhoff, pp. 77-105.
24. Rose L.R.F., and Wang C.H. Analytical methods for designing composite repairs. In: Baker A.A., Rose L.R.F., and Jones R. (Eds). Advances in the Bonded Composite Repair of Metallic Aircraft Structure (2002), Elsevier Chapter 7
25. Schubbe J.J., and Mall S.S. Modelling of cracked thick metallic structure with bonded composite patch repair using three-layer technique. Composite Structures 45 3 (1999) 185-193
26. Volkersen O. Rivet strength distribution in tensile-stressed rivet joints with constant cross-section. Luftfahrforschung 15 1 (1938) 41-47
27. Wang, C.H., Rose, L.R.F., 1997. On the design of bonded patches for one-sided repair. In: Proceedings of the 11th International Conference on Composite materials, Gold Coast, Australia, vol. 5, pp. 347-356.
28. Wang C.H., and Rose L.R.F. Bonded repair of cracks under mixed-mode loading. International Journal of Solids and Structures 35 21 (1998) 2749-2773
29. Wang C.H., and Rose L.R.F. A crack-bridging model for bonded plates subjected to tension and bending. International Journal of Solids and Structures 36 (1999) 1985-2014
30. Wang C.H., Callinan R.J., and Rose L.R.F. Analysis of out-of-plane bending of a one-sided repair. International Journal of Solids and Structures 35 14 (1998) 1653-1675
31. Wen P.H., Aliabadi M.H., and Young A. Boundary element analysis of flat cracked panels with adhesively bonded patches. Engineering Fracture Mechanics 69 (2002) 2129-2147