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- W2369013412 abstract "The study of fatigue property and the analysis of typical crack morphology show that the chemical milling process for aluminium can meet the fatigue design requirement of civil aircraft.The fatigue crack always appears at the radium bottom of the specimen with chemical milling." @default.
- W2369013412 created "2016-06-24" @default.
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- W2369013412 date "2008-01-01" @default.
- W2369013412 modified "2023-09-23" @default.
- W2369013412 title "Fatigue Property of Aluminium Alloy after Chemical Milling" @default.
- W2369013412 hasPublicationYear "2008" @default.
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