To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
- Авторлар: Remizov A.E.1, Vyatkov V.V.1, Osokina E.S.1, Kharchenko R.V.1
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Мекемелер:
- P.A. Soloviev Rybinsk State Aviation Technical University
- Шығарылым: Том 62, № 1 (2019)
- Беттер: 167-170
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230890
- DOI: https://doi.org/10.3103/S1068799819010240
- ID: 230890
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Remizov
P.A. Soloviev Rybinsk State Aviation Technical University
Хат алмасуға жауапты Автор.
Email: ad@rsatu.ru
Ресей, ul. Pushkina 53, Rybinsk, 152934
V. Vyatkov
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Ресей, ul. Pushkina 53, Rybinsk, 152934
E. Osokina
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Ресей, ul. Pushkina 53, Rybinsk, 152934
R. Kharchenko
P.A. Soloviev Rybinsk State Aviation Technical University
Email: ad@rsatu.ru
Ресей, ul. Pushkina 53, Rybinsk, 152934
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