Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer
- Авторы: Tret’yakov V.V.1, Sviridenkov A.A.1, Toktaliev P.D.1
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Учреждения:
- P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
- Выпуск: Том 60, № 3 (2017)
- Страницы: 434-441
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230213
- DOI: https://doi.org/10.3103/S1068799817030163
- ID: 230213
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Аннотация
Features of fuel atomization and propagation in the flow behind a gas-dynamic stabilizer are considered. Estimations of the influence of transverse jets impulse magnitude on characteristics of mixing behind the stabilizer are obtained by numerical and experimental methods.
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Об авторах
V. Tret’yakov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Россия, ul. Aviamotornaya 2, Moscow, 111116
A. Sviridenkov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Россия, ul. Aviamotornaya 2, Moscow, 111116
P. Toktaliev
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Автор, ответственный за переписку.
Email: pavel_d_m@mail.ru
Россия, ul. Aviamotornaya 2, Moscow, 111116
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