Characterization of fatigue behavior of bonded composite repairs

Journal of Aircraft

Volumn 36, Issue 6, 1999, Pages 1016-1022

  Klug, John ^a,b   Maley, Scott ^a   Sun, C T ^a  

^a PURDUE UNIVERSITY   (United States)

^b AEROSPACE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM SHEET; CARBON FIBER REINFORCED PLASTICS; CRACKS; FATIGUE OF MATERIALS; FRACTURE MECHANICS; MATHEMATICAL MODELS; REPAIR; RESIDUAL STRESSES; STRAIN RATE; STRESS INTENSITY FACTORS; THERMAL STRESS;

COMPOSITE PATCHES; MINDLIN PLATE THEORY;

AIRCRAFT MATERIALS;

EID: 0033336375     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2543     Document Type: Article

References (10)

1. Baker, A. A., and Jones, R., Bonded Repair of Aircraft Structure, Martinus Nijhoff, Dordrecht, The Netherlands, 1988.
2. Chue, C., Chang, L., and Tsai, J., "Bonded Repair of a Plate with Inclined Central Crack Under Biaxial Loading," Composite Structures, Vol. 28, 1994, pp. 39-45.
3. Sun, C. T., Klug, J., and Arendt, C., "Analysis of Cracked Aluminum Plates Repaired with Bonded Composite Patches," AIAA Journal, Vol. 34, No. 1, 1996, pp. 369-374.
4. Young, A., Rooke, D. P., and Cartwright, D. J., "Analysis of Patched and Stiffened Cracked Panels Using the Boundary Element Method," International Journal of Solid Structures, Vol. 29, 1992, pp. 2201-2216.
5. Baker, A., "Growth Characterization of Fatigue Cracks Repaired with Adhesively Bonded/Epoxy Patches." Proceedings of the 9th International Conference on Fracture, Advances in Fracture Research, edited by B. L. Karihaloo, Y.-W. Mai, M. I. Ripley, and R. O. Ritchie, Pergamon, New York, Vol. 1, 1977, pp. 117-128.
6. Klug, J., and Sun, C. T., "Large Deflection Effects of Cracked Aluminum Plates Repaired with Bonded Composite Patches," Proceedings of the First International Conference on Composite Science and Technology, Durban, South Africa, June 1996.
7. Rybicki, E., and Kanninen, M., "A Finite Element Calculation of Stress Intensity Factors by a Modified Crack Closure Integral," Engineering Fracture Mechanics, Vol. 9, 1977, pp. 931-938.
8. Belason, E., "Fatigue and Static Ultimate Tests of Boron/Epoxy Doublers Bonded to 7075-6 Aluminum with a Simulated Crack," 18th Symposium of the International Conference on Aeronautical Fatigue, Melbourne, Australia, May 1995.
9. Phillips, P., "Long Crack Growth Rate Data - Constant Amplitude and FALSTAFF Loading," Short-Crack Growth Behavior in an Aluminum Alloy, edited by J. C. Newman, Jr., and P. R. Edwards, AGARD Cooperative Test Programme, Rept. 732, AGARD, 1988, pp. 78-83.
10. Callinan, R. J., Rose, L. R. F., and Wang, C. H., "Three Dimensional Stress Analysis of Crack Patching," Proceedings of the 9th International Conference on Fracture, Advances in Fracture Research, edited by B. L. Karihaloo, Y.-W. Mai, M. I. Ripley, and R. O. Ritchie, Pergamon, New York, Vol. 1, 1977, pp. 2151-2158.