Email this article To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
- Authors: Remizov A.E.1, Vyatkov V.V.1, Osokina E.S.1, Kharchenko R.V.1
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Affiliations:
- P.A. Soloviev Rybinsk State Aviation Technical University
- Issue: Vol 62, No 1 (2019)
- Pages: 167-170
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230890
- DOI: https://doi.org/10.3103/S1068799819010240
- ID: 230890
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Abstract
The paper considers the optimization problems in high-pressure turbine gas-dynamic design based on the ANSYS CFX software package. It is shown that the optimization procedure formation and predicted optimization results depend on the turbine dimension. The best results of the gas-dynamic optimization can be achieved, when turbines with aerodynamically long blades are designed.
About the authors
A. E. Remizov
P.A. Soloviev Rybinsk State Aviation Technical University
Author for correspondence.
Email: ad@rsatu.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
V. V. Vyatkov
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
E. S. Osokina
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
R. V. Kharchenko
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Russian Federation, ul. Pushkina 53, Rybinsk, 152934
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