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Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow. / Lobasov, A. S.; Dekterev, Ar A.; Minakov, A. V.

In: Journal of Physics: Conference Series, Vol. 1382, No. 1, 012059, 28.11.2019.

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

Harvard

Lobasov, AS, Dekterev, AA & Minakov, AV 2019, 'Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow', Journal of Physics: Conference Series, vol. 1382, no. 1, 012059. https://doi.org/10.1088/1742-6596/1382/1/012059

APA

Lobasov, A. S., Dekterev, A. A., & Minakov, A. V. (2019). Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow. Journal of Physics: Conference Series, 1382(1), [012059]. https://doi.org/10.1088/1742-6596/1382/1/012059

Vancouver

Lobasov AS, Dekterev AA, Minakov AV. Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow. Journal of Physics: Conference Series. 2019 Nov 28;1382(1):012059. doi: 10.1088/1742-6596/1382/1/012059

Author

Lobasov, A. S. ; Dekterev, Ar A. ; Minakov, A. V. / Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow. In: Journal of Physics: Conference Series. 2019 ; Vol. 1382, No. 1.

BibTeX

@article{2b8861990703407bbdd446ccea61b503,
title = "Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow",
abstract = "This paper reports on the investigation of combustion features of synthesis gas/air and methane/air flames in a model gas turbine combustor with swirling flow via numerical simulation. This combustor developed for experimental investigation of flow, heat transfer and combustion. For synthesis gas combustion ratio of hydrogen and carbon monoxide was 1:1. The equivalence ratio Φ in both cases was 1.5. The combustor contains systems for water- and air-cooling that provides reasonable temperature value of combustor walls in operating mode. The methane/air flame has the lifted V-shape and synthesis gas/air flame has the columnar tubular flame. In practical, the V-shape flames are more often used. To provide more practical combustion regimes for synthesis gas/air mixture it is necessary to increase the fuel-oxidant mixing efficiency in the premixer of the combustor.",
author = "Lobasov, {A. S.} and Dekterev, {Ar A.} and Minakov, {A. V.}",
year = "2019",
month = nov,
day = "28",
doi = "10.1088/1742-6596/1382/1/012059",
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 - Numerical simulation of synthesis gas/air and methane/air flames for model combustion chamber with swirling flow

AU - Lobasov, A. S.

AU - Dekterev, Ar A.

AU - Minakov, A. V.

PY - 2019/11/28

Y1 - 2019/11/28

N2 - This paper reports on the investigation of combustion features of synthesis gas/air and methane/air flames in a model gas turbine combustor with swirling flow via numerical simulation. This combustor developed for experimental investigation of flow, heat transfer and combustion. For synthesis gas combustion ratio of hydrogen and carbon monoxide was 1:1. The equivalence ratio Φ in both cases was 1.5. The combustor contains systems for water- and air-cooling that provides reasonable temperature value of combustor walls in operating mode. The methane/air flame has the lifted V-shape and synthesis gas/air flame has the columnar tubular flame. In practical, the V-shape flames are more often used. To provide more practical combustion regimes for synthesis gas/air mixture it is necessary to increase the fuel-oxidant mixing efficiency in the premixer of the combustor.

AB - This paper reports on the investigation of combustion features of synthesis gas/air and methane/air flames in a model gas turbine combustor with swirling flow via numerical simulation. This combustor developed for experimental investigation of flow, heat transfer and combustion. For synthesis gas combustion ratio of hydrogen and carbon monoxide was 1:1. The equivalence ratio Φ in both cases was 1.5. The combustor contains systems for water- and air-cooling that provides reasonable temperature value of combustor walls in operating mode. The methane/air flame has the lifted V-shape and synthesis gas/air flame has the columnar tubular flame. In practical, the V-shape flames are more often used. To provide more practical combustion regimes for synthesis gas/air mixture it is necessary to increase the fuel-oxidant mixing efficiency in the premixer of the combustor.

UR - http://www.scopus.com/inward/record.url?scp=85077270679&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1382/1/012059

DO - 10.1088/1742-6596/1382/1/012059

M3 - Conference article

AN - SCOPUS:85077270679

VL - 1382

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012059

T2 - 3th Siberian Thermophysical Seminar, STS 2019

Y2 - 27 August 2019 through 29 August 2019

ER -

ID: 23091783