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- W2376618182 abstract "Aluminum alloy LY12CZ is widely applied in aviation industry.For the low softening tendency under high temperature,it can be used in structures that will serve in high temperature environment.But with temperature increasing,the physical property of the material will suffer from degradation,and the service life will be reduced.The fatigue behavior of the material under various elevated temperature was studied using SEM in-situ technology.The result indicated that elevated temperatures do have impacts on fatigue crack propagation.Based on the micro-cracking investigation,a method to evaluate the fatigue crack growth under combined effect of elevated temperature and mechanical fatigue loads was put forward." @default.
- W2376618182 created "2016-06-24" @default.
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- W2376618182 date "2013-01-01" @default.
- W2376618182 modified "2023-09-27" @default.
- W2376618182 title "Influence of Temperature on Short Fatigue Crack Propagation Behavior of LY12CZ Aluminum" @default.
- W2376618182 hasPublicationYear "2013" @default.
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