电邮这篇文章 Computation of design parameters influence on air injector fuel atomization
- 作者: Sipatov A.M.1, Modorskii V.Y.1, Babushkina A.V.1, Kolodyazhnyi D.Y.2, Nagornyi V.S.2
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隶属关系:
- Perm National Research Polytechnical University
- Peter the Great Saint-Petersburg State Polytechnic University
- 期: 卷 60, 编号 3 (2017)
- 页面: 428-433
- 栏目: 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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详细
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.
作者简介
A. Sipatov
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
俄罗斯联邦, pr. Komsomol’skii 29, Perm, 614990
V. Modorskii
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
俄罗斯联邦, pr. Komsomol’skii 29, Perm, 614990
A. Babushkina
Perm National Research Polytechnical University
编辑信件的主要联系方式.
Email: annvikoz@mail.ru
俄罗斯联邦, pr. Komsomol’skii 29, Perm, 614990
D. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
俄罗斯联邦, Politekhnicheskaya 29, Saint Petersburg, 195251
V. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
俄罗斯联邦, Politekhnicheskaya 29, Saint Petersburg, 195251
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