Email this article Fuel atomization and mixing in unsteady swirling flows behind the gas-dynamic stabilizer
- Authors: Tret’yakov V.V.1, Sviridenkov A.A.1, Toktaliev P.D.1
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Affiliations:
- P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
- Issue: Vol 60, No 3 (2017)
- Pages: 434-441
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230213
- DOI: https://doi.org/10.3103/S1068799817030163
- ID: 230213
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Abstract
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.
Keywords
About the authors
V. V. Tret’yakov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Russian Federation, ul. Aviamotornaya 2, Moscow, 111116
A. A. Sviridenkov
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Email: pavel_d_m@mail.ru
Russian Federation, ul. Aviamotornaya 2, Moscow, 111116
P. D. Toktaliev
P.I. Baranov Central Institute of Aviation Motors Development (TsIAM)
Author for correspondence.
Email: pavel_d_m@mail.ru
Russian Federation, ul. Aviamotornaya 2, Moscow, 111116
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