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
- 作者: Varsegov V.1, Shabalin A.2
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隶属关系:
- Tupolev Kazan National Research Technical University
- All-Russia Research Institute of Flow Metering (FGUP VNIIR)
- 期: 卷 60, 编号 2 (2017)
- 页面: 206-213
- 栏目: 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
如何引用文章
详细
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.
作者简介
V. Varsegov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: varsegov@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. Shabalin
All-Russia Research Institute of Flow Metering (FGUP VNIIR)
Email: varsegov@mail.ru
俄罗斯联邦, ul. Vtoraya Azinskaya 7a, Kazan, 420088 Tatarstan