Fatigue life estimation after crack repair in 6005 A-T6 aluminum alloy using the cold expansion hole technique

Fatigue and Fracture of Engineering Materials and Structures

Volumn 23, Issue 11, 2000, Pages 911-916

  Ghfiri, R ^a   Amrouche, A ^a   Imad, Abdellatif ^b   Mesmacque, G ^a  

^a CNRS   (France)

^b Ecole des Hautes Etudes d'Ingenieur   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; DRILLING; FAILURE ANALYSIS; STRESS CONCENTRATION; STRESS INTENSITY FACTORS;

COLD EXPANSION; HOLE EXPANSION;

CRACK INITIATION;

EID: 0034430290     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2000.00356.x     Document Type: Article

References (18)

1. C. S. Shin, C. M. Wang and P. S. Song (1996) Fatigue damage repair: a comparison of some possible methods. Int. J. Fatigue 18, 525-546.
2. Z. Domazet (1996) Comparison of fatigue crack retardation methods. Engng Failure Anal. 3, 137-147.
3. A. Imad and G. Mesmacque (1988) Retardation Mechanisms of Fatigue Crack Growth Affected by Overloading, Fatigue Crack Growth Under Variable Amplitude Loading (Edited by J. Petit, D. L. Davidson, S. Suresh, P. Rabbe), Elsevier Applied Science, Oxford, UK, pp. 98-108.
4. M. Goto, H. Miyagawa and H. Nisitani (1996) Crack growth arresting property of a hole and brinel-type dimple. Fatigue Fract. Engng. Mater. Struct. 19, 39-49.
5. M. L. Landy, H. J. Armen and H. L. Eidinoff (1986) Enhanced Stop-drill Repair Procedure for Cracked Structures. Fatigue in Mechanically Fastened Composite Metallic Joints. ASTM STP 927, American Society for Testing and Materials, Philadelphia, PA, USA, pp. 190-220.
6. E. E. Peterson (1974) Stress Concentration Factors. John Wiley & Sons, New York, USA.
7. K. Tanaka, Y. Nakai and R. Kawashima (1983) Fracture mechanics approach to fatigue crack initiation from deep notches. Engng Fracture Mech. 18, 1011-23.
8. P. De Rijk and A. A. M. Otter (1971) Empirical Investigation on Some Methods for Stopping the Growth of Fatigue Cracks, Report NLR TR 70021L. National Aerospace Laboratory, The Netherlands.
9. D. L. Ball and D. R. Lowry (1998) Experimental investigation on the effects of cold expansion of fastener boles. Fatigue Fract. Engng Mater. Struct. 21, 17-34.
10. A. Leon (1998) Benefits of split mandrel coldworking. Int. J. Fatigue 20, 1-8.
11. W. H. Cathey and A. F. Grandt (1980) Fracture mechanics consideration of residual stresses introduced by coldworking fastener holes. J. Engng Mater. Technol. 102, 85-91 .
12. M. Bernard, T. Bui-Quoc and M. Burlat (1995) Effect of re-coldworking on fatigue life enhancement of a fastener hole. Fatigue Fract. Engng Mater. Struct. 18, 765-75.
13. C. Ling and X. Zheng (1992) Effects of cold expansion of a fatigue crack initiation location and life of an LY12CZ alloy. Fatigue Fract. Engng Mater. Struct. 15, 241-7.
14. Y. Du-Yi and W. De Jun (1996) A new approach to the prediction of fatigue notch reduction factor kt. Int. J. Fatigue 18, 105-9.
15. A. T. Ozdemir and L. Edwards (1997) Relaxation of residual stresses at cold-worked fastener holes due to fatigue loading. Fatigue Fract. Engng Mater. Struct. 20, 1443-51.
16. R. A. Bell, P. W. Beaver, J. Y. Mann, and J. G. Sparrow (1989) Fatigue of thick-section cold expanded holes with and without cracks. Fatigue Fract. Engng Mater. Struct. 12, 553-67.
17. L. Banks-Sills, E. Dagani, R. Eliasi, E. Reinberg, and R. Schwatzman (1994) Analysis and testing of surface cold-work procedures applied to notched, flat elements. Fatigue Fract. Engng Mater. Struct. 17, 1371-81.
18. ASTM (1988) Standard Test Method for Measurement of Fatigue Crack Growth Rates. ASTM STP E647-88a, American Society for Testing and Materials, Philadelphia, PA, USA.