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Numerical simulation and design of non-uniform arrangement of circular and elliptical holes on the effectiveness of film cooling of a gas turbine blades

Crossref DOI link: https://doi.org/10.1007/s10973-024-13239-9

Published Online: 2024-05-20

Published Print: 2024-05

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

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