Email this article Investigation of Propagation and Orientation of the Turbojet Engine Reverse Jets to Reduce the Ingress of Exhaust Gases to the Engine Inlet
- Authors: Kosterin A.V.1, Lopatin A.A.1, Mingaleev G.F.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 4 (2018)
- Pages: 561-566
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/230704
- DOI: https://doi.org/10.3103/S1068799818040098
- ID: 230704
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Abstract
The results of experimental studies are presented that describe the propagation and orientation of reverse jets in the air cross flow in order to determine design parameters of deflection vane cascade for preventing the ingress of reverse jets in the own or nearby engine.
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About the authors
A. V. Kosterin
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: 89030621520@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. A. Lopatin
Tupolev Kazan National Research Technical University
Email: 89030621520@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
G. F. Mingaleev
Tupolev Kazan National Research Technical University
Email: 89030621520@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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