2020
DOI: 10.1016/j.ijfatigue.2020.105639
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Evaluation of the influence of surface crack-like defects on fatigue life for a P/M nickel-based superalloy FGH96

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Cited by 33 publications
(11 citation statements)
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“…This area is brighter and smoother than the others. Stage II represents the fast crack propagation area, and stage III represents the final fast fracture area 43 . It can be seen that the stage I region of specimen 9 smaller than that of specimens 7 and 8.…”
Section: Results Analysismentioning
confidence: 99%
“…This area is brighter and smoother than the others. Stage II represents the fast crack propagation area, and stage III represents the final fast fracture area 43 . It can be seen that the stage I region of specimen 9 smaller than that of specimens 7 and 8.…”
Section: Results Analysismentioning
confidence: 99%
“…Stage II represents the fast crack propagation area, and stage III represents the final fast fracture area. 44 The stage I area of each specimen shows a semi-circle shape, which suggests that the crack initiated from the surface. Figure 9 demonstrates the crack initiation areas of the specimens with different number of preloading cycles.…”
Section: Methodsmentioning
confidence: 94%
“…The stress level and temperature of the test are based on the maximum stress level and typical temperature at the hot point in turbine discs. 44 The test temperature was 600 C, and the test was conducted in the air environment. The maximum stresses of high and low amplitude loads were designed to be the same value.…”
Section: Methodsmentioning
confidence: 99%
“…The majority of scientifically based approaches to assessing the degree of damage to metal structures are based on models that use the parameters of the limit sizes of crack-like defects [3], the determination of which is a complicated resource-consuming task in the case of the need to predict the durability of materials and structural elements under multi-cycle fatigue. There is a need to develop alternative methods of research that allow obtaining parameters of the limit state of damage of highly stressed metal structures regardless of the limit characteristics of local centers of destruction.…”
Section: Introductionmentioning
confidence: 99%