2014
DOI: 10.1016/j.ijfatigue.2013.04.015
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Influence of mean stress and variable amplitude loading on the fatigue behaviour of a high-strength steel in VHCF regime

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Cited by 64 publications
(58 citation statements)
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“…For example, in the case of VHCF for a medium-carbon structural steel tested by rotary bending (52.5 Hz) in laboratory air with the stress ratio of R = À1, fatigue crack initiated from the subsurface or the interior of specimen with FiE pattern but without FGA morphology [24]. A similar case is the VHCF for a mediumcarbon structural steel tested by ultrasonic axial cycling (21 kHz) in laboratory air with the stress ratios of R = À1 and R = 0, for which cracks nucleated at non-metallic inclusions in the interior of specimen with FiE morphology but FGA was not visible on fracture surfaces [25]. Another interesting case [26] is that, for a high-carbon bearing steel with axial cycling (50 Hz) under the stress ratios of R = 0 and R = 0.5, fatigue cracks initiated from the interior of specimen with FiE pattern and FGA morphology at the failure cycles of 6.22 Â 10 7 at R = 0, whereas the initiation region was with FiE but without FGA morphology at the failure cycles of 2.57 Â 10 5 at R = 0.…”
Section: Introductionmentioning
confidence: 91%
“…For example, in the case of VHCF for a medium-carbon structural steel tested by rotary bending (52.5 Hz) in laboratory air with the stress ratio of R = À1, fatigue crack initiated from the subsurface or the interior of specimen with FiE pattern but without FGA morphology [24]. A similar case is the VHCF for a mediumcarbon structural steel tested by ultrasonic axial cycling (21 kHz) in laboratory air with the stress ratios of R = À1 and R = 0, for which cracks nucleated at non-metallic inclusions in the interior of specimen with FiE morphology but FGA was not visible on fracture surfaces [25]. Another interesting case [26] is that, for a high-carbon bearing steel with axial cycling (50 Hz) under the stress ratios of R = 0 and R = 0.5, fatigue cracks initiated from the interior of specimen with FiE pattern and FGA morphology at the failure cycles of 6.22 Â 10 7 at R = 0, whereas the initiation region was with FiE but without FGA morphology at the failure cycles of 2.57 Â 10 5 at R = 0.…”
Section: Introductionmentioning
confidence: 91%
“…In the crack initiation and early growth stage of VHCF, the crack growth rate is much lower than 10 −10 m/cycle [13,[17][18][19][20]. This indicates that the crack growth in the FGA region occurs first for the most favorable path and does not always extend in all directions in each fatigue cycle.…”
Section: Model and Analysismentioning
confidence: 96%
“…It was shown that the stress intensity factor range at the front of the FGA was a constant and was close to the threshold value of the crack propagation K th . In crack initiation and early growth stage of VHCF, the crack growth rate is much lower than 10 −10 m/cycle [13,[17][18][19][20], and more than 90 % of fatigue life is consumed to form the FGA [21][22][23][24][25]. Therefore, it is essential to develop a model to predict the fatigue life in relation to FGA.…”
Section: Introductionmentioning
confidence: 99%
“…Firstly, a new procedure to rebuild the induction hardening induced residual stress was formulated onto a powered axle made of 34CrNiMo6 steel [16,17]. To derive the remaining life of sampled axles, a fatigue crack growth (FCG) model based on low cycle fatigue (LCF) response from open data was employed [9,18].…”
Section: Introductionmentioning
confidence: 99%