Study on Very-High-Cycle-Fatigue Property of Aero-Engine Blades Based on Subcomponent Specimen

Publisher： Trans Tech Publications

E-ISSN： 1662-9795|2015|664|87-95

ISSN： 1013-9826

Source： Key Engineering Materials, Vol.2015, Iss.664, 2016-01, pp. : 87-95

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