On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct
- Авторы: Remizov A.E.1, Vyatkov V.V.1, Lebedev V.V.1
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Учреждения:
- Rybinsk State Aviation Technical University
- Выпуск: Том 60, № 4 (2017)
- Страницы: 616-620
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230324
- DOI: https://doi.org/10.3103/S1068799817040195
- ID: 230324
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Аннотация
The paper highlights significance of the interturbine transition duct as part of the high pressure and low pressure turbine spool. The correlations have been suggested allowing us to estimate variation of the average cross section flow swirl while its passing the interturbine transition duct.
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Об авторах
A. Remizov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Россия, ul. Pushkina 53, Rybinsk, 152934
V. Vyatkov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Россия, ul. Pushkina 53, Rybinsk, 152934
V. Lebedev
Rybinsk State Aviation Technical University
Автор, ответственный за переписку.
Email: lebedevvlad2000@mail.ru
Россия, ul. Pushkina 53, Rybinsk, 152934
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