Email this article 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
- Authors: Varsegov V.L.1, Shabalin A.S.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- All-Russia Research Institute of Flow Metering (FGUP VNIIR)
- Issue: Vol 60, No 2 (2017)
- Pages: 206-213
- Section: 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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Abstract
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.
About the authors
V. L. Varsegov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: varsegov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111 Tatarstan
A. S. Shabalin
All-Russia Research Institute of Flow Metering (FGUP VNIIR)
Email: varsegov@mail.ru
Russian Federation, ul. Vtoraya Azinskaya 7a, Kazan, 420088 Tatarstan
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