Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
- 作者: Khaliulin R.R.1, Sychenkov V.A.1, Panchenko V.I.1
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隶属关系:
- Tupolev Kazan National Research Technical University
- 期: 卷 61, 编号 1 (2018)
- 页面: 64-70
- 栏目: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230406
- DOI: https://doi.org/10.3103/S1068799818010105
- ID: 230406
如何引用文章
详细
This paper presents the results of an investigation of ejectors with the low entrainment ratio. A technique for calculating the ejectors with a curvilinear axis has been developed. Comparative studies of the performance characteristics of ejectors with the rectilinear axis of the mixing chamber and the curvilinear initial section of the mixing chamber are carried out.
作者简介
R. Khaliulin
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
编辑信件的主要联系方式.
Email: vsychenkov@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Panchenko
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
俄罗斯联邦, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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