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- W2349619104 abstract "Fretting fatigue that exists in the structure of aeronautics is ubiquitous,and has been a focus of the industry.Based on the anti-fretting fatigue experience of Ti1023 main rotor hub central part,this paper introduced the mechanism、influencing factor and anti-fretting fatigue technique of Ti1023,which would give the beneficial reference to other application." @default.
- W2349619104 created "2016-06-24" @default.
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- W2349619104 date "2011-01-01" @default.
- W2349619104 modified "2023-09-28" @default.
- W2349619104 title "Fretting Fatigue of Ti1023 Main Rotor Hub Central Part and Protection" @default.
- W2349619104 hasPublicationYear "2011" @default.
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