Standard

On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners. / Tolstoguzov, R. V.; Sharaborin, D. K.

In: Journal of Physics: Conference Series, Vol. 1382, No. 1, 012067, 28.11.2019.

Research output: Contribution to journal › Conference article › peer-review

Harvard

Tolstoguzov, RV & Sharaborin, DK 2019, 'On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners', Journal of Physics: Conference Series, vol. 1382, no. 1, 012067. https://doi.org/10.1088/1742-6596/1382/1/012067

APA

Tolstoguzov, R. V., & Sharaborin, D. K. (2019). On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners. Journal of Physics: Conference Series, 1382(1), [012067]. https://doi.org/10.1088/1742-6596/1382/1/012067

Vancouver

Tolstoguzov RV, Sharaborin DK. On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners. Journal of Physics: Conference Series. 2019 Nov 28;1382(1):012067. doi: 10.1088/1742-6596/1382/1/012067

Author

Tolstoguzov, R. V. ; Sharaborin, D. K. / On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners. In: Journal of Physics: Conference Series. 2019 ; Vol. 1382, No. 1.

BibTeX

@article{71ed97ca08104b4abfbb8072452af38c,
title = "On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners",
abstract = "This work presents result of visualisation of the characteristic combustion regimes of methane-air and syngas-air swirl-stabilized flames for an unconfined premixed burner (Re = 5000) and non-premixed combustion chamber (Re = 30000). Equivalence ratios were selected to have nearly equal values of the laminar flame propagation speed for the methane/air and syngas/air flames. Visualization for the premixed combustion for the model swirl burner revealed a similar shape of the flames for all mixtures. In contrast, during combustion of methane and syngas in the combustion chamber in the case of combustion in the combustion chamber, these differences in parameters cause completely visually diverse combustion modes.",
keywords = "PRECESSING VORTEX CORE, OSCILLATIONS",
author = "Tolstoguzov, {R. V.} and Sharaborin, {D. K.}",
year = "2019",
month = nov,
day = "28",
doi = "10.1088/1742-6596/1382/1/012067",
language = "English",
volume = "1382",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",
note = "3th Siberian Thermophysical Seminar, STS 2019 ; Conference date: 27-08-2019 Through 29-08-2019",

}

RIS

TY - JOUR

T1 - On combustion regimes of syngas-air and methane-air lean flames for swirl-stabilized burners

AU - Tolstoguzov, R. V.

AU - Sharaborin, D. K.

PY - 2019/11/28

Y1 - 2019/11/28

N2 - This work presents result of visualisation of the characteristic combustion regimes of methane-air and syngas-air swirl-stabilized flames for an unconfined premixed burner (Re = 5000) and non-premixed combustion chamber (Re = 30000). Equivalence ratios were selected to have nearly equal values of the laminar flame propagation speed for the methane/air and syngas/air flames. Visualization for the premixed combustion for the model swirl burner revealed a similar shape of the flames for all mixtures. In contrast, during combustion of methane and syngas in the combustion chamber in the case of combustion in the combustion chamber, these differences in parameters cause completely visually diverse combustion modes.

AB - This work presents result of visualisation of the characteristic combustion regimes of methane-air and syngas-air swirl-stabilized flames for an unconfined premixed burner (Re = 5000) and non-premixed combustion chamber (Re = 30000). Equivalence ratios were selected to have nearly equal values of the laminar flame propagation speed for the methane/air and syngas/air flames. Visualization for the premixed combustion for the model swirl burner revealed a similar shape of the flames for all mixtures. In contrast, during combustion of methane and syngas in the combustion chamber in the case of combustion in the combustion chamber, these differences in parameters cause completely visually diverse combustion modes.

KW - PRECESSING VORTEX CORE

KW - OSCILLATIONS

UR - http://www.scopus.com/inward/record.url?scp=85077264432&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1382/1/012067

DO - 10.1088/1742-6596/1382/1/012067

M3 - Conference article

AN - SCOPUS:85077264432

VL - 1382

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012067

T2 - 3th Siberian Thermophysical Seminar, STS 2019

Y2 - 27 August 2019 through 29 August 2019

ER -

ID: 22994235