journal article·2016-12

On the combination of the critical distance theory with a multiaxial fatigue criterion for predicting the fatigue strength of notched and plain shot-peened parts

M. Benedetti, V. Fontanari, M. Allahkarami, J.C. Hanan, M. Bandini

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Abstract

Abstract Predicting the effect of shot peening on the fatigue life is not an easy task, since it depends on a variety of influence parameters, among them: surface roughness, residual stresses distribution in the peened component and their evolution throughout the service-life, location of the crack initiation site. Indeed, in our experience, preferential crack initiation sites are localized close to the notch root in notched samples and near to edges in prismatic plain specimens. Moreover, the site of crack initiation tends to move sub-superficially with increasing fatigue lifetime. In view of these observations, we believe that a fatigue design method shall take into account the actual external and residual stress field in the neighbourhood of the crack initiation site. For this reason, we suggest using the critical distance theory in the form of an area method to average the stress field in this critical location. Through a numerical/experimental technique, we have estimated the stress field produced by surface peening dimples as well as the residual stress field in the vicinity of sharp edges and notch roots. Stresses were incorporated into a multiaxial fatigue criterion for predicting the S-N curves of peened notched and plain samples made of Al-7075-T651 alloy.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Fatigue and fracture mechanics · Surface Treatment and Residual Stress · Material Properties and Failure Mechanisms

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

References (51)

Show source-provided references
1. Budynas · 2014
2. Hanel · 2003
3. Material fatigue properties for assessing mechanical components weakened by notches and defects10.1111/j.1460-2695.2004.00862.x ↗
4. A fracture mechanics-based approach to estimating the endurance limit of notched components10.1016/j.engfracmech.2015.11.009 ↗
5. A finite-volume-energy based approach to predict the static and the fatigue behaviour of components with sharp V-shaped notches10.1023/A:1013595930617 ↗
6. Some advantages derived from the use of the strain energy density over a control volume in fatigue strength assessments of welded joints10.1016/j.ijfatigue.2007.10.012 ↗
7. Neuber · 1958
8. Notch sensitivity
9. Fatigue design in the presence of stress concentrations10.1243/03093240360713496 ↗
10. A novel formulation of the theory of critical distances to estimate lifetime of notched components in the medium-cycle fatigue regime10.1111/j.1460-2695.2007.01122.x ↗
11. The theory of critical distances to predict static strength of notched brittle components subjected to mixed-mode loading10.1016/j.engfracmech.2007.03.035 ↗
12. A critical distance/plane method to estimate finite life of notched components under variable amplitude uniaxial/multiaxial fatigue loading10.1016/j.ijfatigue.2011.11.015 ↗
13. On the use of the theory of critical distances and the modified Wöhler curve method to estimate fretting fatigue strength of cylindrical contacts10.1016/j.ijfatigue.2006.02.041 ↗
14. Modified Wohler curve method, theory of critical distances and Eurocode 3: a novel engineering procedure to predict the lifetime of steel welded joints subjected to both uniaxial and multiaxial fatigue loading10.1016/j.ijfatigue.2007.06.005 ↗
15. Life assessment methodologies incorporating shot peening process effects; mechanistic consideration of residual stresses and strain hardening. Part 1: the effect of shot peening on fatigue resistance10.1179/1743284713Y.0000000222 ↗
16. Life assessment methodologies incorporating shot peening process effects; mechanistic consideration of residual stresses and strain hardening. Part 2: approaches to fatigue lifing after shot peening10.1179/1743284713Y.0000000223 ↗
17. A comparison of multiaxial fatigue criteria incorporating residual stress effects
18. A model to predict fretting fatigue life including residual stresses10.1016/j.tafmec.2014.06.012 ↗
19. Analysis of the effects of controlled shot peening on fatigue damage of high strength aluminium alloys10.1016/S0142-1123(02)00049-X ↗
20. An analysis of stress concentration caused by shot peening and its application in predicting fatigue strength10.1111/j.1460-2695.1992.tb01262.x ↗
21. Experimental and numerical investigation of material heterogeneity in shot peened aluminium alloy AA2024-T35110.1016/j.surfcoat.2012.12.046 ↗
22. High cycle fatigue behavior prediction of shot-peened parts10.1016/j.ijfatigue.2004.03.007 ↗
23. Fatigue behavior of nitrided and shot peened steel with artificial small surface defects10.1016/j.engfracmech.2012.09.014 ↗
24. Influence of shot peening on bending tooth fatigue limit of case hardened gears10.1016/S0142-1123(02)00034-8 ↗
25. The role of residual stress on the fatigue strength of high performance gearing10.1016/j.ijfatigue.2003.08.014 ↗
26. Fatigue on shot-peened gears: experimentation, simulation and sensitivity analyses10.1111/j.1475-1305.2009.00685.x ↗
27. Schajer · 2013
28. Computational quantification and correction of the errors induced by layer removal for subsurface residual stress measurements10.1016/j.ijmecsci.2012.07.003 ↗
29. Application of different fatigue strength criteria to shot peened notched components. Part 1: fracture mechanics based approaches10.1016/j.apsusc.2013.10.131 ↗
30. A new method for modelling the support effect under rotating bending fatigue: application to Ti-6Al-4V alloy, with and without shot peening10.1111/ffe.12051 ↗
31. The effect of shot peening on notched low cycle fatigue10.1016/j.msea.2011.08.003 ↗
32. Residual stress redistribution in shot peened samples subject to mechanical loading10.1016/j.msea.2014.06.118 ↗
33. Fatigue behaviour of geometric features subjected to laser shock peening: experiments and modelling10.1016/j.ijfatigue.2013.04.016 ↗
34. Experimental and numerical investigation of the effects of shot peening on low-cycle fatigue behaviour of notched geometries
35. Evaluation of residual stresses and strains using the eigenstrain reconstruction method10.1016/j.ijsolstr.2010.03.002 ↗
36. Notch fatigue behaviour of shot peened high-strength aluminium alloys: experiments and predictions using a critical distance method10.1016/j.ijfatigue.2010.02.012 ↗
37. High spatial resolution evaluation of residual stresses in shot peened specimens containing sharp and blunt notches by micro-hole drilling, micro- slot cutting and micro-X-ray diffraction methods10.1007/s11340-016-0182-x ↗
38. Residual stresses reconstruction in shot peened specimens containing sharp and blunt notches by experimental measurements and finite element analysis10.1016/j.ijfatigue.2016.01.020 ↗
39. A simplified and fast method to predict plain and notch fatigue of shot peened high-strength aluminium alloys under reverse bending10.1016/j.surfcoat.2011.12.008 ↗
40. Numerical simulation of residual stress relaxation in shot peened high-strength aluminium alloys under reverse bending fatigue10.1115/1.3184083 ↗
41. Effect of large hydrostatic pressures on the torsional fatigue strength of an alloy steel
42. Multiaxial fatigue resistance of shot peened high-strength aluminum alloys10.1016/j.ijfatigue.2013.10.020 ↗
43. Reverse bending fatigue of shot peened 7075–T651 aluminium alloy: the role of residual stress relaxation10.1016/j.ijfatigue.2008.11.017 ↗
44. Fatigue life enhancement of aluminum alloy for aircraft by fine particle shot peening (FPSP)10.1016/j.jmatprotec.2011.03.011 ↗
45. High- and very high-cycle plain fatigue resistance of shot peened high-strength aluminum alloys: the role of surface morphology10.1016/j.ijfatigue.2014.07.002 ↗
46. Fatigue behavior of shot peened notched specimens: effect of the residual stress field ahead of the notch root10.1016/j.proeng.2015.06.210 ↗
47. Can the conventional high-cycle multiaxial fatigue criteria be re-interpreted in terms of the theory of critical distances?
48. A bi-parametric modified Wöhler curve for high cycle multiaxial fatigue assessment10.1046/j.1460-2695.2002.00462.x ↗
49. A critical plane gradient approach for the prediction of notched HCF life10.1016/j.ijfatigue.2004.10.003 ↗
50. The fatigue behaviour of three-dimensional stress concentrations10.1016/j.ijfatigue.2004.07.006 ↗
51. A two parameter driving force for fatigue crack growth analysis10.1016/j.ijfatigue.2005.07.002 ↗