Randomized trial investigates fatigue behaviors and crack initiation mechanisms in alloy 718 at elevated temperatures, suggesting implications for material performance.
The high‐cycle fatigue (HCF) and very high‐cycle fatigue (VHCF) behaviors of alloy 718 were investigated via ultrasonic axial cycling at room temperature (RT) and 650°C. The lower bound stress amplitude ( σ a ) for survival at 10 9 cycles was 618 MPa at RT and 475 MPa at 650°C. Interestingly, two distinct crack initiation modes were identified at 650°C, leading to significant life differences. When σ a is lower than 520 MPa, single‐crack initiation was observed, triggered by slip‐induced deformation localization. In contrast, when σ a ≥ 520 MPa, multi‐crack initiation was facilitated by deformation localization and stress‐assisted oxidation, where oxygen preferentially reacted with grain boundary δ phases, forming brittle oxides. In addition, fatigue data were incorporated into the modified Yang et al.'s model, showing life factors within ±2.5 for single‐crack initiation samples but ±3.5 for multi‐crack initiation samples. This study emphasized the critical role of stress‐assisted oxidation in high‐temperature life prediction.
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Wang et al. (2026) studied this question.
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