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
- Авторлар: Varsegov V.L.1, Shabalin A.S.2
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Мекемелер:
- Tupolev Kazan National Research Technical University
- All-Russia Research Institute of Flow Metering (FGUP VNIIR)
- Шығарылым: Том 60, № 2 (2017)
- Беттер: 206-213
- Бөлім: 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
Дәйексөз келтіру
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.
Авторлар туралы
V. Varsegov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: varsegov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. Shabalin
All-Russia Research Institute of Flow Metering (FGUP VNIIR)
Email: varsegov@mail.ru
Ресей, ul. Vtoraya Azinskaya 7a, Kazan, 420088 Tatarstan
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