To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
- Autores: Remizov A.E.1, Vyatkov V.V.1, Osokina E.S.1, Kharchenko R.V.1
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Afiliações:
- P.A. Soloviev Rybinsk State Aviation Technical University
- Edição: Volume 62, Nº 1 (2019)
- Páginas: 167-170
- Seção: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230890
- DOI: https://doi.org/10.3103/S1068799819010240
- ID: 230890
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Resumo
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.
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Sobre autores
A. Remizov
P.A. Soloviev Rybinsk State Aviation Technical University
Autor responsável pela correspondência
Email: ad@rsatu.ru
Rússia, ul. Pushkina 53, Rybinsk, 152934
V. Vyatkov
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Rússia, ul. Pushkina 53, Rybinsk, 152934
E. Osokina
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Rússia, ul. Pushkina 53, Rybinsk, 152934
R. Kharchenko
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Rússia, ul. Pushkina 53, Rybinsk, 152934
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