Numerical analysis and experimental validation of the jet impingement cooling of a turbine-blade leading edge at different rotation speeds
A detailed experimental and numerical validation studies are conducted on internal channel jet impingement cooling where seven jets impinging inside a rotating semi-cylindrical channel. The study objective is to mimic the cooling flow structure in gas turbine leading edge by using the rotating the s...
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| Autors principals: | , , , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
Elsevier
2023-11-01
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| Col·lecció: | International Journal of Thermofluids |
| Matèries: | |
| Accés en línia: | http://www.sciencedirect.com/science/article/pii/S2666202723001830 |
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