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Effect of injection hole geometry on film-cooling performance of turbine blades under different free-stream turbulence conditions and blowing ratios

Published Online: 2026-02-17

Authors

Nha, Tuong-Linh

Ta, Viet-Cuong

Dinh, Cong-Truong
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Text and Data Mining valid from 2026-02-17

Version of Record valid from 2026-02-17
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Article History

Received: 28 October 2025

Accepted: 27 January 2026

First Online: 17 February 2026

Declarations

:

: Not applicable.

: Not applicable

: The authors declare no competing interests.

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