Development of the Technique for Calculating the Ejectors with Low Entrainment Ratios
- Авторлар: Khaliulin R.R.1, Sychenkov V.A.1, Panchenko V.I.1
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Мекемелер:
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 64-70
- Бөлім: 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
Дәйексөз келтіру
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.
Авторлар туралы
R. Khaliulin
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Sychenkov
Tupolev Kazan National Research Technical University
Хат алмасуға жауапты Автор.
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan Tatarstan, 420111
V. Panchenko
Tupolev Kazan National Research Technical University
Email: vsychenkov@mail.ru
Ресей, ul. Karla Marksa 10, Kazan Tatarstan, 420111
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