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On the efficiency of using different excitation lines of (1−0) two-line OH fluorescence for planar thermometry. / Lobasov, A. S.; Tolstoguzov, R. V.; Sharaborin, D. K. и др.

в: Thermophysics and Aeromechanics, Том 28, № 5, 09.2021, стр. 751-755.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

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Lobasov AS, Tolstoguzov RV, Sharaborin DK, Chikishev LM, Dulin VM. On the efficiency of using different excitation lines of (1−0) two-line OH fluorescence for planar thermometry. Thermophysics and Aeromechanics. 2021 сент.;28(5):751-755. doi: 10.1134/S0869864321050176

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Lobasov, A. S. ; Tolstoguzov, R. V. ; Sharaborin, D. K. и др. / On the efficiency of using different excitation lines of (1−0) two-line OH fluorescence for planar thermometry. в: Thermophysics and Aeromechanics. 2021 ; Том 28, № 5. стр. 751-755.

BibTeX

@article{bef4ede9ca26423b9e59c88454e7f0d8,
title = "On the efficiency of using different excitation lines of (1−0) two-line OH fluorescence for planar thermometry",
abstract = "The paper presents the results of simulation and experimental study on the efficiency of selecting a pair of excitation lines of OH hydroxyl radical for the (1−0) transition for the A2Σ+−X2Π system for local temperature measurement in a hydrocarbon flame. The LASKIN software was used for the numerical simulation. The temperature field for a laminar methane-air premixed flame (with equivalence ratio equal 1.1) at the atmopsheric pressure was measured. Different combinations of literature-recommended pairs of excitation lines were considered. The results of numerical simulation agree with a theoretical dependency for the temperature range of 1200–2100 K for the coupled excitation lines Q1(5):Q1(14) and Q1(5):Q2(11). However, a moderate discrepancy is observed for the pairs R2(2):R2(13) and R2(2):R2(10). It is concluded that the coupled excitation of Q1(5):Q1(14) and R2(2):R2(13) lines provide a higher sensitivity to the temperature variation. The benefit of the latter pair is that these transitions correspond to close values of the excitation wavelengths in the vicinity of 282 nm. Therefore, this can be convenient for the arrangement of experiments.",
keywords = "hydroxyl radical, laser-induced fluorescence, planar thermometry",
author = "Lobasov, {A. S.} and Tolstoguzov, {R. V.} and Sharaborin, {D. K.} and Chikishev, {L. M.} and Dulin, {V. M.}",
note = "Funding Information: Research was supported by the Ministry of Education and Science of Russia, Agreement No. 075-15-2020-806. Publisher Copyright: {\textcopyright} 2021, A.S. Lobasov, R.B. Tolstoguzov, D.K. Sharaborin, L.M. Chikishev, and V.M. Dulin.",
year = "2021",
month = sep,
doi = "10.1134/S0869864321050176",
language = "English",
volume = "28",
pages = "751--755",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "5",

}

RIS

TY - JOUR

T1 - On the efficiency of using different excitation lines of (1−0) two-line OH fluorescence for planar thermometry

AU - Lobasov, A. S.

AU - Tolstoguzov, R. V.

AU - Sharaborin, D. K.

AU - Chikishev, L. M.

AU - Dulin, V. M.

N1 - Funding Information: Research was supported by the Ministry of Education and Science of Russia, Agreement No. 075-15-2020-806. Publisher Copyright: © 2021, A.S. Lobasov, R.B. Tolstoguzov, D.K. Sharaborin, L.M. Chikishev, and V.M. Dulin.

PY - 2021/9

Y1 - 2021/9

N2 - The paper presents the results of simulation and experimental study on the efficiency of selecting a pair of excitation lines of OH hydroxyl radical for the (1−0) transition for the A2Σ+−X2Π system for local temperature measurement in a hydrocarbon flame. The LASKIN software was used for the numerical simulation. The temperature field for a laminar methane-air premixed flame (with equivalence ratio equal 1.1) at the atmopsheric pressure was measured. Different combinations of literature-recommended pairs of excitation lines were considered. The results of numerical simulation agree with a theoretical dependency for the temperature range of 1200–2100 K for the coupled excitation lines Q1(5):Q1(14) and Q1(5):Q2(11). However, a moderate discrepancy is observed for the pairs R2(2):R2(13) and R2(2):R2(10). It is concluded that the coupled excitation of Q1(5):Q1(14) and R2(2):R2(13) lines provide a higher sensitivity to the temperature variation. The benefit of the latter pair is that these transitions correspond to close values of the excitation wavelengths in the vicinity of 282 nm. Therefore, this can be convenient for the arrangement of experiments.

AB - The paper presents the results of simulation and experimental study on the efficiency of selecting a pair of excitation lines of OH hydroxyl radical for the (1−0) transition for the A2Σ+−X2Π system for local temperature measurement in a hydrocarbon flame. The LASKIN software was used for the numerical simulation. The temperature field for a laminar methane-air premixed flame (with equivalence ratio equal 1.1) at the atmopsheric pressure was measured. Different combinations of literature-recommended pairs of excitation lines were considered. The results of numerical simulation agree with a theoretical dependency for the temperature range of 1200–2100 K for the coupled excitation lines Q1(5):Q1(14) and Q1(5):Q2(11). However, a moderate discrepancy is observed for the pairs R2(2):R2(13) and R2(2):R2(10). It is concluded that the coupled excitation of Q1(5):Q1(14) and R2(2):R2(13) lines provide a higher sensitivity to the temperature variation. The benefit of the latter pair is that these transitions correspond to close values of the excitation wavelengths in the vicinity of 282 nm. Therefore, this can be convenient for the arrangement of experiments.

KW - hydroxyl radical

KW - laser-induced fluorescence

KW - planar thermometry

UR - http://www.scopus.com/inward/record.url?scp=85123457910&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/3d4442b0-f17d-388e-b309-f1c1ad177f05/

U2 - 10.1134/S0869864321050176

DO - 10.1134/S0869864321050176

M3 - Article

AN - SCOPUS:85123457910

VL - 28

SP - 751

EP - 755

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 5

ER -

ID: 35347477