Email this article Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
- Authors: Khaliulin R.R.1, Sychenkov V.A.1, Panchenko V.I.1
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Affiliations:
- Tupolev Kazan National Research Technical University
- Issue: Vol 61, No 1 (2018)
- Pages: 64-70
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journal-vniispk.ru/1068-7998/article/view/230406
- DOI: https://doi.org/10.3103/S1068799818010105
- ID: 230406
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Abstract
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.
About the authors
R. R. Khaliulin
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. A. Sychenkov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. I. Panchenko
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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