Email this article Model study of conditions, when the reverse jet ingests into the engine input located behind the wing
- Authors: Mingaleev G.F.1, Margulis S.G.2, Kosterin A.V.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- OAO Ural Works of Civil Aviation
- Issue: Vol 59, No 4 (2016)
- Pages: 543-547
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/229897
- DOI: https://doi.org/10.3103/S1068799816040164
- ID: 229897
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Abstract
This paper presents the results of the model studies of the reverse jet distribution limits in the air cross-flow, performed in the wind tunnel, as well as the conditions of the jet’s ingestion into the engine air intake in the context of aircraft configuration, when the engines are the input of engines.
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About the authors
G. F. Mingaleev
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: mingaleevgaziz@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
S. G. Margulis
OAO Ural Works of Civil Aviation
Email: mingaleevgaziz@mail.ru
Russian Federation, ul. Belinskogo 262M, Ekaterinburg, 620089
A. V. Kosterin
Tupolev Kazan National Research Technical University
Email: mingaleevgaziz@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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