Standard

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

In: Thermophysics and Aeromechanics, Vol. 24, No. 3, 01.05.2017, p. 347-353.

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

Harvard

Chikishev, LM, Dulin, VM, Gobyzov, OA, Lobasov, AS & Markovich, DM 2017, 'Mixing in a model gas turbine combustor studied by panoramic optical techniques', Thermophysics and Aeromechanics, vol. 24, no. 3, pp. 347-353. https://doi.org/10.1134/S0869864317030039

APA

Chikishev, L. M., Dulin, V. M., Gobyzov, O. A., Lobasov, A. S., & Markovich, D. M. (2017). Mixing in a model gas turbine combustor studied by panoramic optical techniques. Thermophysics and Aeromechanics, 24(3), 347-353. https://doi.org/10.1134/S0869864317030039

Vancouver

Chikishev LM, Dulin VM, Gobyzov OA, Lobasov AS, Markovich DM. Mixing in a model gas turbine combustor studied by panoramic optical techniques. Thermophysics and Aeromechanics. 2017 May 1;24(3):347-353. doi: 10.1134/S0869864317030039

Author

Chikishev, L. M. ; Dulin, V. M. ; Gobyzov, O. A. et al. / Mixing in a model gas turbine combustor studied by panoramic optical techniques. In: Thermophysics and Aeromechanics. 2017 ; Vol. 24, No. 3. pp. 347-353.

BibTeX

@article{58bd07ae1ab54fb2b56c1443d1c297c4,
title = "Mixing in a model gas turbine combustor studied by panoramic optical techniques",
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",
month = may,
day = "1",
doi = "10.1134/S0869864317030039",
language = "English",
volume = "24",
pages = "347--353",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "3",

}

RIS

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

UR - http://www.scopus.com/inward/record.url?scp=85026888439&partnerID=8YFLogxK

U2 - 10.1134/S0869864317030039

DO - 10.1134/S0869864317030039

M3 - Article

AN - SCOPUS:85026888439

VL - 24

SP - 347

EP - 353

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 3

ER -

ID: 10069701