2021
DOI: 10.1016/j.ijmecsci.2021.106591
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Characteristic and mechanism of crack initiation and early growth of an additively manufactured Ti-6Al-4V in very high cycle fatigue regime

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Cited by 54 publications
(19 citation statements)
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“…Around the initiation site, there was an obvious semicircular FGA, forming the initiation characteristic area (ICA) of the surface initiation. This finding was different from the results obtained in the earlier studies, which proposed that the FGA was absent if the fatigue crack initiated from the specimen surface 43,44 . Magnified morphology inside the FGA is presented in Figure 4B, which shows the existence of a relatively smooth region outside the initiation site.…”
Section: Resultscontrasting
confidence: 91%
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“…Around the initiation site, there was an obvious semicircular FGA, forming the initiation characteristic area (ICA) of the surface initiation. This finding was different from the results obtained in the earlier studies, which proposed that the FGA was absent if the fatigue crack initiated from the specimen surface 43,44 . Magnified morphology inside the FGA is presented in Figure 4B, which shows the existence of a relatively smooth region outside the initiation site.…”
Section: Resultscontrasting
confidence: 91%
“…After the fatigue cracks initiated from the surface, repeated contact of the fracture surface along the crack led to the formation of the FGA and fisheye, 18 which overturns the previous conclusion that FGA and fish‐eye morphology can only be found in the internal initiation. Sun et al 43 found that the fracture surface presented a fish‐eye‐like pattern along with an FGA morphology in the interior when the fatigue cracks initiated from the inside of the material. In contrast, the FGA and fish‐eye morphologies disappeared in surface initiation mode under the rotating bending fatigue test or the ultrasonic frequency fatigue test.…”
Section: Discussionmentioning
confidence: 99%
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“…Recently, there are results regarding the VHCF behavior of AM titanium alloys (Ti6Al4V) 59–66 and AlSi10Mg alloys 67–73 . Fatigue damage in VHCF behavior occurs between 10 7 and 10 9 cycles 61 .…”
Section: Factors Affecting Fatigue Strength and Behavior In Ammentioning
confidence: 99%
“…57 It has been stated in the literature that the level of surface roughness is inversely proportional to the fatigue strength. 21,58 Recently, there are results regarding the VHCF behavior of AM titanium alloys (Ti6Al4V) [59][60][61][62][63][64][65][66] and AlSi10Mg alloys. [67][68][69][70][71][72][73] Fatigue damage in VHCF behavior occurs between 10 7 and 10 9 cycles.…”
Section: Factors Affecting Fatigue Strength and Behavior In Ammentioning
confidence: 99%