Enviar artigo por via de e-mail Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
- Autores: Remizov A.1, Vyatkov V.1, Lebedev V.1
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Afiliações:
- Rybinsk State Aviation Technical University
- Edição: Volume 59, Nº 4 (2016)
- Páginas: 559-564
- Seção: 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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Resumo
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.
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Sobre autores
A. Remizov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Rússia, Ulitsa Pushkina,53, Rybinsk, 152934
V. Vyatkov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Rússia, Ulitsa Pushkina,53, Rybinsk, 152934
V. Lebedev
Rybinsk State Aviation Technical University
Autor responsável pela correspondência
Email: lebedevvlad2000@mail.ru
Rússia, Ulitsa Pushkina,53, Rybinsk, 152934
