电邮这篇文章 Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
- 作者: Remizov A.1, Vyatkov V.1, Lebedev V.1
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隶属关系:
- Rybinsk State Aviation Technical University
- 期: 卷 59, 编号 4 (2016)
- 页面: 559-564
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229909
- DOI: https://doi.org/10.3103/S106879981604019X
- ID: 229909
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详细
Methods to control flow have been considered in order to reduce end losses in blade rows of GTE gas turbines by means of measures taken at the design stage.
作者简介
A. Remizov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
俄罗斯联邦, Ulitsa Pushkina,53, Rybinsk, 152934
V. Vyatkov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
俄罗斯联邦, Ulitsa Pushkina,53, Rybinsk, 152934
V. Lebedev
Rybinsk State Aviation Technical University
编辑信件的主要联系方式.
Email: lebedevvlad2000@mail.ru
俄罗斯联邦, Ulitsa Pushkina,53, Rybinsk, 152934
