Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer
- Авторлар: Tret’yakov V.V.1, Sviridenkov A.A.1, Toktaliev P.D.1
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Мекемелер:
- P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 434-441
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230213
- DOI: https://doi.org/10.3103/S1068799817030163
- ID: 230213
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
V. Tret’yakov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Ресей, ul. Aviamotornaya 2, Moscow, 111116
A. Sviridenkov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Ресей, ul. Aviamotornaya 2, Moscow, 111116
P. Toktaliev
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Хат алмасуға жауапты Автор.
Email: pavel_d_m@mail.ru
Ресей, ul. Aviamotornaya 2, Moscow, 111116
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