Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
Spatial Structure of a Reacting Turbulent Swirling Jet Flow with Combustion of a Propane–Air Mixture. / Sharaborin, D. K.; Markovich, D. M.; Dulin, V. M.
в: Combustion, Explosion and Shock Waves, Том 54, № 3, 01.05.2018, стр. 294-300.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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TY - JOUR
T1 - Spatial Structure of a Reacting Turbulent Swirling Jet Flow with Combustion of a Propane–Air Mixture
AU - Sharaborin, D. K.
AU - Markovich, D. M.
AU - Dulin, V. M.
N1 - Publisher Copyright: © 2018, Pleiades Publishing, Ltd.
PY - 2018/5/1
Y1 - 2018/5/1
N2 - Results of an experimental study of the spatial structure of a reacting flow during combustion of a propane–air mixture in a turbulent swirling jet escaping into atmospheric air are presented. The fuel-to-air equivalence ratio is φ = 0.7, and the Reynolds number of the jet is Re = 5 · 103. The time-averaged spatial distributions of velocity, local density, and concentrations of the main species of the gas mixture are measured in low-swirl and high-swirl flows. In both cases, the flame front is stabilized in the internal mixing layer formed by the axial region of jet retardation, where hot combustion products are concentrated. In a high-swirl flow, the temperature distributions in the cross section y/d = 0.5 show that the region with the maximum temperature of the gas is located at the periphery of the central recirculation zone. Moreover, in the case of a high-swirl flow, there exists a recirculation zone at the axis, and the CO2 concentration is twice higher than in a low-swirl jet. The opposite situation is observed for O2.
AB - Results of an experimental study of the spatial structure of a reacting flow during combustion of a propane–air mixture in a turbulent swirling jet escaping into atmospheric air are presented. The fuel-to-air equivalence ratio is φ = 0.7, and the Reynolds number of the jet is Re = 5 · 103. The time-averaged spatial distributions of velocity, local density, and concentrations of the main species of the gas mixture are measured in low-swirl and high-swirl flows. In both cases, the flame front is stabilized in the internal mixing layer formed by the axial region of jet retardation, where hot combustion products are concentrated. In a high-swirl flow, the temperature distributions in the cross section y/d = 0.5 show that the region with the maximum temperature of the gas is located at the periphery of the central recirculation zone. Moreover, in the case of a high-swirl flow, there exists a recirculation zone at the axis, and the CO2 concentration is twice higher than in a low-swirl jet. The opposite situation is observed for O2.
KW - flame in a swirling flow
KW - particle image velocimetry
KW - spontaneous Raman scattering
KW - PARTICLE IMAGE VELOCIMETRY
KW - LASER
KW - BURNER
KW - TEMPERATURE-MEASUREMENTS
KW - FLAME
KW - DIAGNOSTICS
UR - http://www.scopus.com/inward/record.url?scp=85048055990&partnerID=8YFLogxK
U2 - 10.1134/S001050821803005X
DO - 10.1134/S001050821803005X
M3 - Article
AN - SCOPUS:85048055990
VL - 54
SP - 294
EP - 300
JO - Combustion, Explosion and Shock Waves
JF - Combustion, Explosion and Shock Waves
SN - 0010-5082
IS - 3
ER -
ID: 13755148