Mixing in a model gas turbine combustor studied by panoramic optical techniques

L. M. Chikishev; V. M. Dulin; O. A. Gobyzov; A. S. Lobasov; D. M. Markovich

doi:10.1134/S0869864317030039

Mixing in a model gas turbine combustor studied by panoramic optical techniques

L. M. Chikishev, V. M. Dulin, O. A. Gobyzov, A. S. Lobasov, D. M. Markovich

Результат исследования: Научные публикации в периодических изданиях › статья › рецензирование

1 Цитирования (Scopus)

Аннотация

Using planar optical methods based on laser-induced fluorescence and particle image velocimetry instantaneous velocity fields and passive tracer concentration are measured simultaneously in a model of GT-combustor at realistic flow rates. Spatial distributions of velocity pulsations and passive tracer concentration pulsations are measured at air flow rate about 0.4 kg/s. Correlations of velocity and concentration pulsations are measured. The most intense turbulent mass flux in the region of swirling flow mixing layer was observed. The contribution of advective and turbulent components in the transfer of a passive tracer in the axial direction was estimated.

Язык оригинала	английский
Страницы (с-по)	347-353
Число страниц	7
Журнал	Thermophysics and Aeromechanics
Том	24
Номер выпуска	3
DOI	https://doi.org/10.1134/S0869864317030039
Состояние	Опубликовано - 1 мая 2017

Доступ к документу

10.1134/S0869864317030039

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abstract = "Using planar optical methods based on laser-induced fluorescence and particle image velocimetry instantaneous velocity fields and passive tracer concentration are measured simultaneously in a model of GT-combustor at realistic flow rates. Spatial distributions of velocity pulsations and passive tracer concentration pulsations are measured at air flow rate about 0.4 kg/s. Correlations of velocity and concentration pulsations are measured. The most intense turbulent mass flux in the region of swirling flow mixing layer was observed. The contribution of advective and turbulent components in the transfer of a passive tracer in the axial direction was estimated.",

keywords = "acetone vapor, gas turbine combustor, laser-induced fluorescence, particle image velocimetry, passive tracer concentration, turbulent flow",

author = "Chikishev, {L. M.} and Dulin, {V. M.} and Gobyzov, {O. A.} and Lobasov, {A. S.} and Markovich, {D. M.}",

year = "2017",

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Mixing in a model gas turbine combustor studied by panoramic optical techniques. / Chikishev, L. M.; Dulin, V. M.; Gobyzov, O. A.; Lobasov, A. S.; Markovich, D. M.

В: Thermophysics and Aeromechanics, Том 24, № 3, 01.05.2017, стр. 347-353.

Результат исследования: Научные публикации в периодических изданиях › статья › рецензирование

TY - JOUR

T1 - Mixing in a model gas turbine combustor studied by panoramic optical techniques

AU - Chikishev, L. M.

AU - Dulin, V. M.

AU - Gobyzov, O. A.

AU - Lobasov, A. S.

AU - Markovich, D. M.

PY - 2017/5/1

Y1 - 2017/5/1

N2 - Using planar optical methods based on laser-induced fluorescence and particle image velocimetry instantaneous velocity fields and passive tracer concentration are measured simultaneously in a model of GT-combustor at realistic flow rates. Spatial distributions of velocity pulsations and passive tracer concentration pulsations are measured at air flow rate about 0.4 kg/s. Correlations of velocity and concentration pulsations are measured. The most intense turbulent mass flux in the region of swirling flow mixing layer was observed. The contribution of advective and turbulent components in the transfer of a passive tracer in the axial direction was estimated.

AB - Using planar optical methods based on laser-induced fluorescence and particle image velocimetry instantaneous velocity fields and passive tracer concentration are measured simultaneously in a model of GT-combustor at realistic flow rates. Spatial distributions of velocity pulsations and passive tracer concentration pulsations are measured at air flow rate about 0.4 kg/s. Correlations of velocity and concentration pulsations are measured. The most intense turbulent mass flux in the region of swirling flow mixing layer was observed. The contribution of advective and turbulent components in the transfer of a passive tracer in the axial direction was estimated.

KW - acetone vapor

KW - gas turbine combustor

KW - laser-induced fluorescence

KW - particle image velocimetry

KW - passive tracer concentration

KW - turbulent flow

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JO - Thermophysics and Aeromechanics

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