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Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner. / Yusupov, Roman; Shtork, Sergey; Alekseenko, Sergey.

In: EPJ Web of Conferences, Vol. 159, 0052, 25.10.2017.

Research output: Contribution to journal › Article › peer-review

Harvard

Yusupov, R, Shtork, S & Alekseenko, S 2017, 'Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner', EPJ Web of Conferences, vol. 159, 0052. https://doi.org/10.1051/epjconf/201715900052

APA

Yusupov, R., Shtork, S., & Alekseenko, S. (2017). Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner. EPJ Web of Conferences, 159, [0052]. https://doi.org/10.1051/epjconf/201715900052

Vancouver

Yusupov R, Shtork S, Alekseenko S. Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner. EPJ Web of Conferences. 2017 Oct 25;159:0052. doi: 10.1051/epjconf/201715900052

Author

Yusupov, Roman ; Shtork, Sergey ; Alekseenko, Sergey. / Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner. In: EPJ Web of Conferences. 2017 ; Vol. 159.

BibTeX

@article{cc0a78638e974b2099f1ea3c305a4705,
title = "Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner",
abstract = "The work deals with the experimental study of the aerodynamic structure of a swirling flow in the isothermal model of two-stage vortex combustion chamber. The main attention is focused on the process of flow mixing of two successively connected tangential swirlers of the first and second stages of the working section. Data on flow visualization are presented for two patterns of flow swirling. Time-averaged profiles of the axial and tangential velocity components are obtained with the help of laser-Doppler anemometer. In the case of flow co-swirling between two stages of the working section, instability of a secondary flow in the form of precessing vortex was distinguished. For the regime with counter flow swirling, effective mixing of the swirl flows was found; this was reflected by formation of the flow with uniform distribution of axial velocity over the cross-section.",
author = "Roman Yusupov and Sergey Shtork and Sergey Alekseenko",
note = "Publisher Copyright: {\textcopyright} The authors, published by EDP Sciences, 2017.",
year = "2017",
month = oct,
day = "25",
doi = "10.1051/epjconf/201715900052",
language = "English",
volume = "159",
journal = "EPJ Web of Conferences",
issn = "2101-6275",
publisher = "EDP Sciences",

}

RIS

TY - JOUR

T1 - Isothermal modeling of aerodynamic structure of the swirling flow in a two-stage burner

AU - Yusupov, Roman

AU - Shtork, Sergey

AU - Alekseenko, Sergey

N1 - Publisher Copyright: © The authors, published by EDP Sciences, 2017.

PY - 2017/10/25

Y1 - 2017/10/25

N2 - The work deals with the experimental study of the aerodynamic structure of a swirling flow in the isothermal model of two-stage vortex combustion chamber. The main attention is focused on the process of flow mixing of two successively connected tangential swirlers of the first and second stages of the working section. Data on flow visualization are presented for two patterns of flow swirling. Time-averaged profiles of the axial and tangential velocity components are obtained with the help of laser-Doppler anemometer. In the case of flow co-swirling between two stages of the working section, instability of a secondary flow in the form of precessing vortex was distinguished. For the regime with counter flow swirling, effective mixing of the swirl flows was found; this was reflected by formation of the flow with uniform distribution of axial velocity over the cross-section.

AB - The work deals with the experimental study of the aerodynamic structure of a swirling flow in the isothermal model of two-stage vortex combustion chamber. The main attention is focused on the process of flow mixing of two successively connected tangential swirlers of the first and second stages of the working section. Data on flow visualization are presented for two patterns of flow swirling. Time-averaged profiles of the axial and tangential velocity components are obtained with the help of laser-Doppler anemometer. In the case of flow co-swirling between two stages of the working section, instability of a secondary flow in the form of precessing vortex was distinguished. For the regime with counter flow swirling, effective mixing of the swirl flows was found; this was reflected by formation of the flow with uniform distribution of axial velocity over the cross-section.

UR - http://www.scopus.com/inward/record.url?scp=85033473644&partnerID=8YFLogxK

U2 - 10.1051/epjconf/201715900052

DO - 10.1051/epjconf/201715900052

M3 - Article

AN - SCOPUS:85033473644

VL - 159

JO - EPJ Web of Conferences

JF - EPJ Web of Conferences

SN - 2101-6275

M1 - 0052

ER -

ID: 8970651