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- W2553547219 abstract "Ultrasonic fatigue tests were carried out to investigate the effect of stress ratio on the very high cycle fatigue (VHCF) behaviors of titanium alloy (Ti-8Al-1Mo-1V). The fatigue strength at stress ratios of 0.1 and 0.5 were lower than the safely modified Goodman approximation, and a significant deviation was observed in the VHCF regime. Based on fractography and fracture mechanics, the fatigue failure process was congruously divided into four stages: (1) crack initiation induced by cleavage of primary α grains and its coalescence; (2) microstructure-sensitive slow crack propagation; (3) microstructure-insensitive fast crack propagation; and (4) final fatigue failure. Meanwhile, for surface crack initiation, fatigue crack propagation life only occupied less than 3% of total life in the VHCF regime, and over 95% of the fatigue crack propagation life was expended in the microstructure-sensitive crack propagation stage. The effect of stress ratio on crack propagation life was not distinct." @default.
- W2553547219 created "2016-11-30" @default.
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- W2553547219 date "2017-06-01" @default.
- W2553547219 modified "2023-10-16" @default.
- W2553547219 title "Very high cycle fatigue behaviors of a turbine engine blade alloy at various stress ratios" @default.
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- W2553547219 doi "https://doi.org/10.1016/j.ijfatigue.2016.11.032" @default.
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