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Thermo-mechanical fatigue characteristics of CMSX-4 applied to the high-pressure turbine first-stage single-crystal rotor blade

Crossref DOI link: https://doi.org/10.1007/s12206-020-0406-y

Published Online: 2020-04-30

Published Print: 2020-05

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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