2008
DOI: 10.1016/j.ijfatigue.2007.08.011
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Estimation of the size of GBF area on fracture surface for high strength steels in very high cycle fatigue regime

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Cited by 56 publications
(42 citation statements)
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“…For all the 17 groups of experimental data shown in Fig. 6, the experimental value is close to its mean value [34] GCr15 [24] 50CrV4 [33] 54SiCrV6 [33] G [35] GVM [35] GER [35] SUJ2 [14] QT1 [33] Number of cycles to failure 6 Ratio of experimental value K FGA to mean value K FGA versus fatigue life for present experimental data and those from the literature, in which the superscripts 1 and 2 denote the specimens by oil-quenching and tempering for 2.5 h in a vacuum at 150 • C under an ultrasonic test and a conventional frequency test, respectively, and the superscripts 3 and 4 denote the specimens by oil-quenching and tempering for 2.5 h in a vacuum at 300 • C under an ultrasonic test and a conventional frequency test, respectively GCr15 [34] GCr15 [24] 50CrV4 [33] 54SiCrV6 [33] G Experimental FGA size (μm) Fig. 7 Estimated FGA sizes as a function of the experimental data for each group of experimental results in Fig.…”
Section: Fga Size Estimationsupporting
confidence: 52%
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“…For all the 17 groups of experimental data shown in Fig. 6, the experimental value is close to its mean value [34] GCr15 [24] 50CrV4 [33] 54SiCrV6 [33] G [35] GVM [35] GER [35] SUJ2 [14] QT1 [33] Number of cycles to failure 6 Ratio of experimental value K FGA to mean value K FGA versus fatigue life for present experimental data and those from the literature, in which the superscripts 1 and 2 denote the specimens by oil-quenching and tempering for 2.5 h in a vacuum at 150 • C under an ultrasonic test and a conventional frequency test, respectively, and the superscripts 3 and 4 denote the specimens by oil-quenching and tempering for 2.5 h in a vacuum at 300 • C under an ultrasonic test and a conventional frequency test, respectively GCr15 [34] GCr15 [24] 50CrV4 [33] 54SiCrV6 [33] G Experimental FGA size (μm) Fig. 7 Estimated FGA sizes as a function of the experimental data for each group of experimental results in Fig.…”
Section: Fga Size Estimationsupporting
confidence: 52%
“…Consider a mode-I internal penny crack with diameter d in an infinite solid under a uniform remote tensile stress σ , the maximum size of the plastic zone r p under the plane strain condition is [33] …”
Section: Model and Analysismentioning
confidence: 99%
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“…Chai [13] reported that the formation of subsurface non-defect fatigue crack was caused by a material damage process of soft phase due to cyclic plastic deformation. Yang et al [23] measured the FGA of two spring steels and proposed a criterion to estimate the size of FGA. Hong et al [24] performed tests of a high carbon chromium steel and calculated fatigue life from FGA to fish-eye and from fish-eye to the critical crack size.…”
Section: Introductionmentioning
confidence: 99%
“…The superscript asterisk in Fig. 7b denotes the experimental data by Murakami et al obtained from the reference by Yang et al [30], the superscripts 1 and 2 in Fig. 7g and h denote the specimens oilquenched and tempered for 2.5 h in vacuum at 300°C with furnace-cooling under ultrasonic test and conventional frequency test, respectively.…”
Section: Fatigue Strength Model and Analysismentioning
confidence: 99%