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AERODYNAMIC ENHANCEMENT IN INNER CHANNEL OF TURBINE BLADE
This paper presents the numerical and experimental study of the flow structure in a radial cooling passage model of a gas turbine blade. The investigations focus on the flow aerodynamics in the channel, which is an accurate representation of the configuration used in aero engines. The flow structur...
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| Main Authors: | , , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Gdańsk University of Technology
2015-04-01
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| Colecção: | TASK Quarterly |
| Assuntos: | |
| Acesso em linha: | https://journal.mostwiedzy.pl/TASKQuarterly/article/view/1876 |
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