2019
DOI: 10.1016/j.msea.2019.02.075
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Investigation on low-cycle fatigue behaviors of wrought superalloy GH4742 at room-temperature and 700 °C

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Cited by 19 publications
(10 citation statements)
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“…Multiple fatigue crack initiation occurred, and the fracture surfaces were dimple-like, indicating transgranular fatigue crack propagation, typical for superalloys at room temperature. 11,13,16,37 The extensive surface roughening by PSMs (see Figure 7C) with numerous cracks starting from the PSMs and following an active slip plane (Figure 7D,E) agrees with previous investigations. 11,13,16,37 The occurrence of PSMs, as well as the underlying PSBs, is a manifestation of the localized cyclic plastic straining of the material.…”
Section: Fatigue Damage and Fatigue Life At Room Temperaturesupporting
confidence: 90%
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“…Multiple fatigue crack initiation occurred, and the fracture surfaces were dimple-like, indicating transgranular fatigue crack propagation, typical for superalloys at room temperature. 11,13,16,37 The extensive surface roughening by PSMs (see Figure 7C) with numerous cracks starting from the PSMs and following an active slip plane (Figure 7D,E) agrees with previous investigations. 11,13,16,37 The occurrence of PSMs, as well as the underlying PSBs, is a manifestation of the localized cyclic plastic straining of the material.…”
Section: Fatigue Damage and Fatigue Life At Room Temperaturesupporting
confidence: 90%
“…11,13,16,37 The extensive surface roughening by PSMs (see Figure 7C) with numerous cracks starting from the PSMs and following an active slip plane (Figure 7D,E) agrees with previous investigations. 11,13,16,37 The occurrence of PSMs, as well as the underlying PSBs, is a manifestation of the localized cyclic plastic straining of the material. The initiation of the fatigue cracks in room temperature fatigue of René 41 superalloy is strongly dependent on plastic strain amplitude.…”
Section: Fatigue Damage and Fatigue Life At Room Temperaturesupporting
confidence: 90%
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“…The fracture morphologies of the LCF samples with different strain amplitudes of 0.2% and 0.6% at 700 °C are exhibited in Figure 12 . Figure 12 shows the typical characteristics with the three regions comprising the fatigue source, fatigue crack propagation zone and final fracture zone [ 19 ]. It can be seen from Figure 12 that when the strain amplitude increased from 0.2% to 0.6%, the crack propagation area decreased, the number of crack initiation sources of the novel steel was less than that of the 30SiMn2MoV steel and the crack propagation area was greater than that of 30SiMn2MoV steel with the same strain amplitude.…”
Section: Resultsmentioning
confidence: 99%