Email this article Computation of design parameters influence on air injector fuel atomization
- Authors: Sipatov A.M.1, Modorskii V.Y.1, Babushkina A.V.1, Kolodyazhnyi D.Y.2, Nagornyi V.S.2
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Affiliations:
- Perm National Research Polytechnical University
- Peter the Great Saint-Petersburg State Polytechnic University
- Issue: Vol 60, No 3 (2017)
- Pages: 428-433
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230207
- DOI: https://doi.org/10.3103/S1068799817030151
- ID: 230207
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Abstract
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.
About the authors
A. M. Sipatov
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
Russian Federation, pr. Komsomol’skii 29, Perm, 614990
V. Ya. Modorskii
Perm National Research Polytechnical University
Email: annvikoz@mail.ru
Russian Federation, pr. Komsomol’skii 29, Perm, 614990
A. V. Babushkina
Perm National Research Polytechnical University
Author for correspondence.
Email: annvikoz@mail.ru
Russian Federation, pr. Komsomol’skii 29, Perm, 614990
D. Yu. Kolodyazhnyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
Russian Federation, Politekhnicheskaya 29, Saint Petersburg, 195251
V. S. Nagornyi
Peter the Great Saint-Petersburg State Polytechnic University
Email: annvikoz@mail.ru
Russian Federation, Politekhnicheskaya 29, Saint Petersburg, 195251
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