On the characterization of fatigue crack growth in a plate with a single-sided repair

Journal of Engineering Materials and Technology

Volumn 126, Issue 2, 2004, Pages 192-198

  Duong, C N ^a   Wang, C H ^b  

^a BOEING COMPANY   (United States)

^b DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; PLATES (STRUCTURAL COMPONENTS); REPAIR; STRESS CONCENTRATION; STRESS INTENSITY FACTORS; STRUCTURAL PANELS;

COMPOSITE BONDED REPAIRS; CRACK LENGTH; FATIGUE CRACK GROWTH; LOAD-PATH ECCENTRICITY;

CRACK PROPAGATION;

EID: 12344257819     PISSN: 00944289     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1647129     Document Type: Article

References (13)

1. Baker, A. A., Jones, R., Rose, F., and Rao, K. J., 2002, Advances in the Bonded Composite Repair of Metallic Aircraft Structures, Elsevier Publisher, The Netherlands.
2. Ratwani, M. M., 1979, "Analysis of Cracked, Adhesively Bonded Laminate Structures," AIAA J., 17, pp. 988-994.
3. Rose, L. R. F., 1988, "Theoretical Analysis of Crack Patching," in Bonded Repair of Aircraft Structures, A. A. Baker and R. Jones, eds., Martinus Nijhoff, New York.
4. Ratwani, M. M., 1980, "A Parametric Study of Fatigue Crack Growth Behavior in Adhesively Bonded Metallic Structures," ASME J. Eng. Mater. Technol., 100, pp. 46-51.
5. Arendt, C., and Sun, C. T., 1994, "Bending Effects of Unsymmetric Adhesively Bonded Composite Repairs on Cracked Aluminum Panels," Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, NASA Conference Publication 3274, Part 1, pp. 33-48.
6. Wang, C. H., Rose, L. R. F., and Callinan, R., 1998, "Analysis of Out-of-Plane Bending in One-Sided Bonded Repair," Int. J. Solids Struct., 35, pp. 1653-1675.
7. Wang, C. H., and Rose, L. R. F., 1999, "A Crack Bridging Model for Bonded Plates Subjected to Tension and Bending," Int. J. Solids Struct., 36, pp. 1985-2014.
8. Beom, H. G., and Earmme, Y. Y., 1999, "The Elastic Field of an Elliptic Cyclindrical Inclusion in a Laminate With Multiple Isotropic Layers," ASME J. Appl. Mech., 66, pp. 165-171.
9. Duong, C. N., and Yu, J., 2003, "Analysis of a Plate Containing a Polygon-Shaped Inclusion With a Uniform Eigencurvature," ASME J. Appl. Mech., 70, pp. 404-407.
10. Duong, C. N., and Yu, J., 2003, "Thermal Stresses in a One-Sided Bonded Repair: An Approximate Geometrically Nonlinear Analysis," Theor. Appl. Fract. Mech. J., 40, pp. 197-209.
11. Duong, C. N., 2004, "An Engineering Approach to Geometrically Nonlinear Analysis of a One-Sided Bonded Repair Under Thermo-Mechanical Loading," Compos. Struct., 64, pp. 13-21.
12. Duong, C. N., 2003, Composite Repair of Aircraft Structures, Program Report, Volume III: Tests and Method Validations, prepared for USAF Air Force Research Laboratory.
13. De Koning, A. U., 1980, "A Simple Crack Closure Model for Prediction of Fatigue Crack Growth Rates Under Variable Amplitude Loading," NRL MP 80006.