Мақаланы E-mail арқылы жіберу Computation of design parameters influence on air injector fuel atomization
- Авторлар: Sipatov A.M.1, Modorskii V.Y.1, Babushkina A.V.1, Kolodyazhnyi D.Y.2, Nagornyi V.S.2
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Мекемелер:
- Perm National Research Polytechnical University
- Peter the Great Saint-Petersburg State Polytechnic University
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 428-433
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230207
- DOI: https://doi.org/10.3103/S1068799817030151
- ID: 230207
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Аннотация
A technique for calculating the two-phase flows at liquid fuel atomization by the air injector is developed. In the course of numerical experiments, the flow parameter distributions over the cross section and volume for different nozzle design options are obtained. The influence of the twist angle of the gas flow on the liquid fuel atomization is analyzed.
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Авторлар туралы
A. Sipatov
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
Ресей, pr. Komsomol’skii 29, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
Ресей, pr. Komsomol’skii 29, Perm, 614990
A. Babushkina
Perm National Research Polytechnical University
Хат алмасуға жауапты Автор.
Email: annvikoz@mail.ru
Ресей, pr. Komsomol’skii 29, Perm, 614990
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
Ресей, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
Ресей, Politekhnicheskaya 29, Saint Petersburg, 195251
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