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Calculated study of tangential inclination of nozzle vanes influence on gas-dynamic efficiency of axial turbine stage
- Authors: Baturin O.V.1, Matveev V.N.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 3 (2008): Special Issue
- Pages: 114-118
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/620
- DOI: https://doi.org/10.18287/2541-7533-2008-0-3(16)-114-118
- ID: 620
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Abstract
The result of calculated study are stated and the changes of flow and losses structure in vane rows in transonic turbine stage by the tangential inclination of nozzle vanes have been justified in given article. Recommendations on the choice of bent vanes shape of the nozzle vane row have been suggested.
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About the authors
O. V. Baturin
Samara State Aerospace University
Author for correspondence.
Email: matveev.vn@ssau.ru
Russian Federation
V. N. Matveev
Samara State Aerospace University
Email: matveev.vn@ssau.ru
Russian Federation
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