2019
DOI: 10.1016/j.ijfatigue.2019.105229
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A microstructure based approach to model effects of surface roughness on tensile fatigue

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Cited by 35 publications
(9 citation statements)
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“…Much research on the fatigue behavior of superalloys revealed that surface roughness has a strong influence on fatigue life, 4–6 especially when high cycle fatigue is considered. Stress concentration introduced by the rough surface significantly affects the fatigue lives of the materials 7–13 . In addition, surface stress caused by surface oxides may also lead to surface crack initiation 14 .…”
Section: Introductionmentioning
confidence: 99%
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“…Much research on the fatigue behavior of superalloys revealed that surface roughness has a strong influence on fatigue life, 4–6 especially when high cycle fatigue is considered. Stress concentration introduced by the rough surface significantly affects the fatigue lives of the materials 7–13 . In addition, surface stress caused by surface oxides may also lead to surface crack initiation 14 .…”
Section: Introductionmentioning
confidence: 99%
“…Stress concentration introduced by the rough surface significantly affects the fatigue lives of the materials. [7][8][9][10][11][12][13] In addition, surface stress caused by surface oxides may also lead to surface crack initiation. 14 Although the original cast components might have different surface states and internal microstructures as a result of a unique manufacturing process such as the thin structures in the current work that resemble contemporary high-pressure turbine blades, there is no open literature discussing the fatigue of these components.…”
Section: Introductionmentioning
confidence: 99%
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“…It is well-known that the fatigue life is also sensitive to geometric discontinuity such as notch. This topic has already been studied (e.g., Deng et al, 2015;Ferjaoui et al, 2015;Kumar et al, 2018;Singh et al, 2019;Zhan et al, 2017). Recently, investigated the effect of micro-notch size on crack initiation in LCF from an experimental and numerical perspective.…”
Section: Introduction and General Scopementioning
confidence: 99%
“…A main motivation to carry out this research work is that no studies have been developed concerning the effect of pre-corrosion on the fatigue endurance, under conventional and ultrasonic tests, on this aeronautical aluminum alloy. Concerning surface roughness, fatigue life has been studied in a carbon steel, showing that this superficial parameter influences fatigue life only during crack initiation Metals 2020, 10, 1033 2 of 17 stage [14]; others investigations [15,16], have referred that fatigue life is reduced with the increase of roughness. In this study, the roughness has been registered before and after the conventional fatigue tests, in order to record its variation.…”
Section: Introductionmentioning
confidence: 99%