Modeling of a cracked metallic structure with bonded composite patch using the three layer technique

Composite Structures

Volumn 35, Issue 3, 1996, Pages 295-308

  Naboulsi, S ^a   Mall, S ^a  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; BONDING; COMPUTER SIMULATION; CRACKS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); STRAIN RATE; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS;

BONDED COMPOSITE PATCH; CRACKED METALLIC STRUCTURE; STRAIN ENERGY RELEASE RATE; THREE LAYER TECHNIQUE;

COMPOSITE STRUCTURES;

EID: 0030197458     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/0263-8223(96)00043-8     Document Type: Article

References (27)

1. Baker, A. A., A summary of work on applications of advanced fiber components at the Aeronautical Research Lab. J. Composite, 9 (1987) 11-16.
2. Baker, A. A., Callinan, R. J., Davis, M. J., Jones, R. & Williams, J. F., Repair of Mirage III aircraft using BFRP crack patching technique. Theor. Appl. Fracture Mech., 2 (1984) 1-16.
3. Baker, A. A. & Jones, R., Bonded Repair of Aircraft Structures, chaps 4 and 5. Martinus Nijhoff Publishers, 1988.
4. Jones, R., Bonded repair of damage. J. Aero. Soc. (India), 36 (1984) 193-201.
5. Jones, R., Davis, M. J., Callinan, R. J. & Mallinson, G., Crack patching analysis and design. J. Struct. Mech., 10 (1982) 177-90.
6. Rose, L. R. F., An application of the inclusion analogy for bonded reinforcements. Int. J. Solids Struct., 17 (1981) 827-38.
7. Rose, L. R. F., A cracked plate repaired by bonded reinforcements. Int. J. Fract., 18 (1982) 135-44.
8. Muki, R. & Sternberg, E., On the analysis of overlapping bonded elastic sheets. Int. J. Solids Struct., 4 (1968) 75-94.
9. Ratwani, M. M., A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures. J. Engng Materials Technol., 100 (1978) 46-51.
10. Ratwani, M. M., Analysis of cracked adhesively bonded laminated structures. AIAA J., 17 (1979) 988-94.
11. Ratwani, M. M., Characterization of fatigue crack growth in bonded structures-analysis of cracked bonded structures. Air Force Flight Dynamics Laboratory AFFADL-TR-31, Vol. II, July 1977.
12. Ratwani, M. M., Characterization of fatigue crack growth in bonded structures-crack growth predictions in bonded structures. Air Force Flight Dynamics Laboratory AFFADL-TR-77-31, Vol. I, July 1977.
13. Tong, P., Pian, T. H. H. & Lasry, S. J., A hybrid element approach to crack problems in plane elasticity. Int. J. Numer. Meth. Engng, 7 (1973) 297-308.
14. Sun, C. T. & Arendt, C., Bending effects of unsymmetric adhesively bonded composite repairs on cracked aluminium panels. In Proc. FAA/NASA Int. Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, Vol. Part I, 1994.
15. Sun, C. T., Klug, J. & Arendt, C., Analysis of cracked aluminum plates repaired by bonded composite patches. AIAA J., 34 (1996) 369-74.
16. Rybicki, E. F. & Kanninen, E. F., A finite element calculation of stress intensity factors by a modified crack closure integral. Engng Fracture Mech., 9 (1977) 931-8.
17. Young, M. J. & Sun, C. T., On the strain energy release rate for a cracked plate subjected to out-of-plane bending moment. Int. J. Fract., 60 (1993) 227-47.
18. Chue, C. H., Chang, L. C. & Tsai, J. S., Bonded repair of a plate with inclined central crack under biaxial loading. Composite Struct., 28 (1994) 39-45.
19. Whitcomb, J. D., Three-dimensional analysis of a postbuckled embedded delamination. J. Composite Mater., 23 (1989) 862-89.
20. Whitcomb, J. D., Three-dimensional analysis of a postbuckled embedded delamination. In NASA TP 2823. NASA, 1988.
21. Irwin, G. R., Fracture. Handbuch Physik, 6 (1958) 551.
22. Klug, J., Wu, X. X. & Sun, C. T., Efficient modeling of delamination growth in composite laminates using plate elements. In Symposium on the Durability of Composite Materials, ed. R. C. Wetherhold, Vol. 51. ASME Publications, Maryland, 1994, pp. 177-89.
23. Young, M. J., Rooke, D. P. & Cartwright, D. J., Analysis of patched and stiffened cracked panels using the boundary element method. Int. J. Solids Struct., 29 (17) (1992) 2201-16.
24. Dattaguru, B., Everett, R. A., Jr, Whitcomb, J. D. & Johnson, W. S., Geometrically nonlinear analysis of adhesively bonded joints. J. Engng Mater. Technol., 106 (1984) 59-65.
25. Poole, P., Lock, D. & Young, A., Composite patch repair of thick aluminum alloy sections. In International Conference on Aircraft Damage Assessment and Repair, Melbourne, Australia, 1991, pp. 85-91. Institute of Engineers, Australia.
26. Baker, A. A., Fatigue crack propagation studies on aluminum panels patched with boron/epoxy composites. In International Conference on Aircraft Damage Assessment and Repair, Melbourne, Australia, 1991, pp. 209-15. Institute of Engineers, Australia.
27. Denney, J. J. & Mall, S., Effect of disbond on fatigue behavior of cracked aluminum panel with bonded composite patch. AIAA J., submitted.