电邮这篇文章 Model study of conditions, when the reverse jet ingests into the engine input located behind the wing
- 作者: Mingaleev G.F.1, Margulis S.G.2, Kosterin A.V.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- OAO Ural Works of Civil Aviation
- 期: 卷 59, 编号 4 (2016)
- 页面: 543-547
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229897
- DOI: https://doi.org/10.3103/S1068799816040164
- ID: 229897
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详细
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.
作者简介
G. Mingaleev
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: mingaleevgaziz@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
S. Margulis
OAO Ural Works of Civil Aviation
Email: mingaleevgaziz@mail.ru
俄罗斯联邦, ul. Belinskogo 262M, Ekaterinburg, 620089
A. Kosterin
Tupolev Kazan National Research Technical University
Email: mingaleevgaziz@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
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