journal article·2010-04

On the prediction of the residual fatigue life of cracked structures repaired by the stop-hole method

Hao Wu, Abdellatif Imad, Noureddine Benseddiq, Jaime Tupiassú Pinho de Castro, Marco Antonio Meggiolaro

International Journal of Fatigue· Volume 32· Issue 4
Publisher page

Abstract

The stop-hole method is a simple and economic repair technique widely used to retard or even to stop the propagation of a fatigue crack in structural components that cannot be replaced immediately after the detection of the crack. Its principle is to drill a hole at or close to the crack tip to transform the crack into a notch, reducing in this way its stress concentration effect. The fatigue life increment that can be achieved with this technique can be modeled by assuming that it is equal to the number of cycles required to re-initiate the crack at the resulting notch root, which depends at least on the crack size and on the hole diameter. The aim of the present work is to predict the fatigue crack initiation lives by employing classical eN concepts properly modified by short crack theory to model the stop-hale effect. The comparison among the experimental and the calculation results show that the life increment caused by the stop-holes can be effectively predicted in this way.
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Research context

OpenAlex topics: Fatigue and fracture mechanics · Non-Destructive Testing Techniques · Ultrasonics and Acoustic Wave Propagation

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (25)

Show source-provided references
1. Fatigue life estimation after crack repair in 6005 AT-6 aluminium alloy using the cold expansion hole technique10.1046/j.1460-2695.2000.00356.x ↗
2. Stop drilling procedure for fatigue life improvement10.1016/j.ijfatigue.2004.04.009 ↗
3. Comparison of fatigue crack retardation methods10.1016/1350-6307(96)00006-4 ↗
4. Validation of crack arrest technique by numerical modeling10.1016/S0142-1123(97)00008-X ↗
5. A crack-growth arresting technique in aluminum alloy10.1016/j.engfailanal.2007.02.005 ↗
6. Peterson · 1974
7. Shigley · 2004
8. Juvinall · 2005
9. Norton · 2005
10. Dowling · 1999
11. Short crack threshold estimates to predict notch sensitivity factors in fatigue10.1016/j.ijfatigue.2007.02.022 ↗
12. E647 Standard test method for measurement of fatigue crack growth rates. ASTM Standards; 2006. [accessed 03.01.06].
13. E399 Standard method of test for plain strain fracture toughness of metallic materials. ASTM Standards; 2006. [accessed 03.01.06].
14. Evaluation of overload effects on fatigue crack growth and closure10.1016/S0013-7944(02)00119-4 ↗
15. Meggiolaro MA, Castro JTP. Evaluation of the errors induced by high nominal stresses in the classical εN method. In: 8th International fatigue congress, Stockholm, Sweden, FATIGUE; 2002. pp. 2759–2766.
16. Fatigue crack propagation under complex loading in arbitrary 2D geometries
17. Prediction of non-propagating cracks10.1016/0013-7944(79)90081-X ↗
18. On the possible generalizations of the Kitagawa–Takahashi diagram and of the El Haddad equation to finite life10.1016/j.ijfatigue.2005.12.001 ↗
19. Scaling of quasibrittle fracture: the fractal hypothesis, its critique and Weibull connection10.1023/A:1007335506684 ↗
20. Frost · 1974
21. Tada · 1985
22. Juvinall · 1967
23. Stephens · 2000
24. 1997
25. Fatigue failure of a hydraulic filter head10.1016/S1350-6307(01)00029-2 ↗