Отправить статью по E-mail Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser
- Авторы: Varsegov V.1, Shabalin A.2
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Учреждения:
- Tupolev Kazan National Research Technical University
- All-Russia Research Institute of Flow Metering (FGUP VNIIR)
- Выпуск: Том 60, № 2 (2017)
- Страницы: 206-213
- Раздел: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230076
- DOI: https://doi.org/10.3103/S1068799817020076
- ID: 230076
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Аннотация
The work comprises numerical investigation of the influence of the deflection angles of the trailing edges of longitudinal ribs on the gas-dynamic behavior of vane cascades of a thrust reverser located in the secondary flow of a bypass turbofan engine (BTFE). Verification of the numerical model was performed on the basis of experimental research.
Об авторах
V. Varsegov
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: varsegov@mail.ru
Россия, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. Shabalin
All-Russia Research Institute of Flow Metering (FGUP VNIIR)
Email: varsegov@mail.ru
Россия, ul. Vtoraya Azinskaya 7a, Kazan, 420088 Tatarstan
