Email this article Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
- Authors: Remizov A.E.1, Vyatkov V.V.1, Lebedev V.A.1
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Affiliations:
- Rybinsk State Aviation Technical University
- Issue: Vol 59, No 4 (2016)
- Pages: 559-564
- Section: 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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Abstract
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.
About the authors
A. E. Remizov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Russian Federation, Ulitsa Pushkina,53, Rybinsk, 152934
V. V. Vyatkov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Russian Federation, Ulitsa Pushkina,53, Rybinsk, 152934
V. A. Lebedev
Rybinsk State Aviation Technical University
Author for correspondence.
Email: lebedevvlad2000@mail.ru
Russian Federation, Ulitsa Pushkina,53, Rybinsk, 152934
