电邮这篇文章 3D Investigations of the High Pressure Turbine Vane Platform Convection Cooling and Convection-Film Cooling
- 作者: Gorelov Y.G.1, Anan’ev V.V.1
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隶属关系:
- Salyut Gas Turbine Engineering Research and Production Center
- 期: 卷 61, 编号 3 (2018)
- 页面: 452-459
- 栏目: 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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详细
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.
作者简介
Yu. Gorelov
Salyut Gas Turbine Engineering Research and Production Center
编辑信件的主要联系方式.
Email: Yury.Dina@gmail.com
俄罗斯联邦, pr. Budennogo 16, Moscow, 105118
V. Anan’ev
Salyut Gas Turbine Engineering Research and Production Center
Email: Yury.Dina@gmail.com
俄罗斯联邦, pr. Budennogo 16, Moscow, 105118
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