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Study on the Residual Stress in Film-Cooled Turbine Blade-Thermal Barrier Coating System with 3D Finite Element Model

Crossref DOI link: https://doi.org/10.1007/s11666-025-01977-7

Published Online: 2025-03-06

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

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