Enviar artigo por via de e-mail 3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling
- Autores: Gorelov Y.G.1, Anan’ev V.V.1
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Afiliações:
- Salyut Gas Turbine Engineering Research and Production Center
- Edição: Volume 61, Nº 3 (2018)
- Páginas: 452-459
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230640
- DOI: https://doi.org/10.3103/S1068799818030200
- ID: 230640
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Resumo
3D ANSYS CFX conjugate calculation was carried out to compare cooling effectiveness of the high pressure turbine vane platforms with the film cooling and the convection-film cooling.
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Sobre autores
Yu. Gorelov
Salyut Gas Turbine Engineering Research and Production Center
Autor responsável pela correspondência
Email: Yury.Dina@gmail.com
Rússia, pr. Budennogo 16, Moscow, 105118
V. Anan’ev
Salyut Gas Turbine Engineering Research and Production Center
Email: Yury.Dina@gmail.com
Rússia, pr. Budennogo 16, Moscow, 105118
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