Modeling of cracked thick metallic structure with bonded composite patch repair using three-layer technique

Composite Structures

Volumn 45, Issue 3, 1999, Pages 185-193

  Schubbe, J J ^a   Mall, S ^a  

^a Air Force Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOND STRENGTH (MATERIALS); CRACK PROPAGATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS;

COMPOSITE PATCH REPAIR;

COMPOSITE STRUCTURES;

EID: 0032668081     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(99)00025-2     Document Type: Article

References (22)

1. Baker AA, Jones R, editors. Bonded Repair of Aircraft Structures, Martinus Nijhoff Publishers, 1988.
2. Baker AA. Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches, Fatigue & Fracture of Engineering Materials & Structures. 1993;16(7):753-765.
3. Ratwani MM. A parametric study of fatigue crack growth behavior in adhesively bonded metallic structures, Journal of Engineering Materials and Technology 1978;100:46-51.
4. Ratwani MM. Analysis of cracked adhesively bonded laminated structure, AIAA Journal 1979;17:988-994.
5. Denney JJ, Mall S. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch, Engineering Fracture Mechanics 1997;57(5):507-525.
6. Fredell R, Barneveld WV, Vlot A. Analysis of composite patching of fuselage structures: High patch elastic modulus isn't the whole story. Proceedings of the 39th International SAMPE Symposium, Anaheim, CA, vol. I, 610-623, April 11-14, 1994.
7. Naboulsi S, Mall S. Modeling of a cracked metallic structure with bonded composite patch using the three-layer technique, Composite Structures 1996;35(3):295-308.
8. Naboulsi S, Mall S. Thermal effects on adhesively bonded composite patch repair of cracked aluminum panels, Theoretical and Applied Fracture Mechanics 1997;26:1-12.
9. Naboulsi S, Mall S. Characterization of fatigue crack growth in aluminum panels with bonded composite patch, Composite Structures 1997;37(3-4)321-334.
10. Naboulsi S, Mall S. Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches, Theoretical and Applied Fracture Mechanics 1997;28:13-28.
11. Kan HP, Ratwani MM. Composite patch repair of thick aluminum structures-final report, Airtask No. WF41-400, PE 62241, Report No. NADC-82139-60, United States Navy-Naval Air Development Center, Warminster, PA 18974, 1983.
12. Jones R, Moment L, Baker AA, Davis MJ. Bonded repair of metallic components: Thick sections, Theoretical and Applied Fracture Mechanics 1988;9:61-70.
13. Heller M, Hill TG, Williams JF, Jones R. Increasing the fatigue life of cracked fastener holes using bonded repairs, Theoretical and Applied Fracture Mechanics 1989;11:1-8.
14. Labor JD, Ratwani MM. Development of bonded composite patch repairs for cracked metal structure-Final report. Report No. NADC-79066-60, Vol. 1, United States Navy-Naval Air Development Center, Warminster, PA 18974, 1980.
15. Molent L, Callinan RJ, Jones R. Structural aspects of the design of an all boron/epoxy reinforcement for the F 111C wing pivot fitting, Journal of Composite Structures 1989;11(1):57-83.
16. Damage tolerance and fatigue evaluation of structures, federal aviation administration advisory circular 1986;25.571-A.
17. Jones R, Chiu WK, Smith R. Airworthiness of composite repairs: Failure mechanisms, Engineering Failure Analysis 1995;2(2):117-128.
18. ASTM Standard E647, Measurement of fatigue crack growth rates, American Society for Testing and Materials, Philadelphia, PA, 1990.
19. Sun CT, Krug J, Arendt C. Analysis of cracked aluminum plates repaired with bonded composite patches, AIAA Journal 1996;34:369-374.
20. Rybicki EF, Kanninen EF. A finite element calculation of stress intensity factors by a modified crack closure integral, Engineering Fracture Mechanics 1977;9:931-938.
21. Young MJ, Sun CT. On the strain energy release rate for a cracked plate subjected to out-of-plane bending moment, International Journal of Fatigue 1993;60:227-247.
22. Schubbe JJ. Thickness effects on a cracked aluminum plate with composite patch repair, Ph.D. Thesis, Air Force Institute of Technology, 1997.