Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
- Авторы: Khaliulin R.R.1, Sychenkov V.A.1, Panchenko V.I.1
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Учреждения:
- Tupolev Kazan National Research Technical University
- Выпуск: Том 61, № 1 (2018)
- Страницы: 64-70
- Раздел: 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
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Аннотация
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.
Об авторах
R. Khaliulin
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Автор, ответственный за переписку.
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Panchenko
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Россия, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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