Email this article On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct
- Authors: Remizov A.E.1, Vyatkov V.V.1, Lebedev V.V.1
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Affiliations:
- Rybinsk State Aviation Technical University
- Issue: Vol 60, No 4 (2017)
- Pages: 616-620
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230324
- DOI: https://doi.org/10.3103/S1068799817040195
- ID: 230324
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Abstract
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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About the authors
A. E. Remizov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
V. V. Vyatkov
Rybinsk State Aviation Technical University
Email: lebedevvlad2000@mail.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
V. V. Lebedev
Rybinsk State Aviation Technical University
Author for correspondence.
Email: lebedevvlad2000@mail.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
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