Development of a turbulence dissipation based reaction rate model for progress variable in turbulent premixed flames

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Development of a turbulence dissipation based reaction rate model for progress variable in turbulent premixed flames. / Tomasch, Stefanie; Swaminathan, Nedunchezhian; Spijker, Christoph et al.
In: Combustion theory and modelling, Vol. 26.2022, No. 5, 16.06.2022, p. 896-915.

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Tomasch S, Swaminathan N, Spijker C, Ertesvåg IS. Development of a turbulence dissipation based reaction rate model for progress variable in turbulent premixed flames. Combustion theory and modelling. 2022 Jun 16;26.2022(5):896-915. Epub 2022 Jun 16. doi: 10.1080/13647830.2022.2083525

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@article{d57b986c21424025acc814bdf764971d,
title = "Development of a turbulence dissipation based reaction rate model for progress variable in turbulent premixed flames",
abstract = "This study presents an algebraic combustion closure for Large eddy simulation (LES) exhibiting attributes of simplicity and simultaneous accuracy under realistic combustion conditions. The model makes use of the interlink between the reaction and dissipation rates in premixed turbulent combustion but relaxes the thin flame assumption by considering finite-rate chemistry effects in the small-scale turbulence structure. The core idea of the approach is to approximate the reaction progress in the unresolved spectrum of wave lengths and to use it within a filtered reaction rate expression. The model is implemented in OpenFOAM 4.0 and is tested on a turbulent, premixed flame behind a bluff-body, applying an LES approach for turbulence modelling. The cross comparison of velocity, temperature and composition data with experiments and a well-investigated combustion model in literature reveals competitive performance of the new model. Especially in the near-field of the bluff body flame, corresponding to thin and moderately thickened flame regions, its ability to capture the flame structure is highly promising. The chosen, partly explicit approach to recover the temperature from the transported sensible enthalpy, involving a strong coupling between filtered reaction and heat release rate, also shows advantages over obtaining the temperature from presumed probability density functions.",
keywords = "CFD, combustion, LES, progress variable, subgrid scale",
author = "Stefanie Tomasch and Nedunchezhian Swaminathan and Christoph Spijker and Ertesv{\aa}g, {Ivar S.}",
note = "Publisher Copyright: {\textcopyright} 2022 The Author(s). Published by Informa UK Limited, trading as Taylor & Francis Group.",
year = "2022",
month = jun,
day = "16",
doi = "10.1080/13647830.2022.2083525",
language = "English",
volume = "26.2022",
pages = "896--915",
journal = "Combustion theory and modelling",
issn = "1364-7830",
number = "5",

}

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TY - JOUR

T1 - Development of a turbulence dissipation based reaction rate model for progress variable in turbulent premixed flames

AU - Tomasch, Stefanie

AU - Swaminathan, Nedunchezhian

AU - Spijker, Christoph

AU - Ertesvåg, Ivar S.

N1 - Publisher Copyright: © 2022 The Author(s). Published by Informa UK Limited, trading as Taylor & Francis Group.

PY - 2022/6/16

Y1 - 2022/6/16

N2 - This study presents an algebraic combustion closure for Large eddy simulation (LES) exhibiting attributes of simplicity and simultaneous accuracy under realistic combustion conditions. The model makes use of the interlink between the reaction and dissipation rates in premixed turbulent combustion but relaxes the thin flame assumption by considering finite-rate chemistry effects in the small-scale turbulence structure. The core idea of the approach is to approximate the reaction progress in the unresolved spectrum of wave lengths and to use it within a filtered reaction rate expression. The model is implemented in OpenFOAM 4.0 and is tested on a turbulent, premixed flame behind a bluff-body, applying an LES approach for turbulence modelling. The cross comparison of velocity, temperature and composition data with experiments and a well-investigated combustion model in literature reveals competitive performance of the new model. Especially in the near-field of the bluff body flame, corresponding to thin and moderately thickened flame regions, its ability to capture the flame structure is highly promising. The chosen, partly explicit approach to recover the temperature from the transported sensible enthalpy, involving a strong coupling between filtered reaction and heat release rate, also shows advantages over obtaining the temperature from presumed probability density functions.

AB - This study presents an algebraic combustion closure for Large eddy simulation (LES) exhibiting attributes of simplicity and simultaneous accuracy under realistic combustion conditions. The model makes use of the interlink between the reaction and dissipation rates in premixed turbulent combustion but relaxes the thin flame assumption by considering finite-rate chemistry effects in the small-scale turbulence structure. The core idea of the approach is to approximate the reaction progress in the unresolved spectrum of wave lengths and to use it within a filtered reaction rate expression. The model is implemented in OpenFOAM 4.0 and is tested on a turbulent, premixed flame behind a bluff-body, applying an LES approach for turbulence modelling. The cross comparison of velocity, temperature and composition data with experiments and a well-investigated combustion model in literature reveals competitive performance of the new model. Especially in the near-field of the bluff body flame, corresponding to thin and moderately thickened flame regions, its ability to capture the flame structure is highly promising. The chosen, partly explicit approach to recover the temperature from the transported sensible enthalpy, involving a strong coupling between filtered reaction and heat release rate, also shows advantages over obtaining the temperature from presumed probability density functions.

KW - CFD

KW - combustion

KW - LES

KW - progress variable

KW - subgrid scale

UR - http://www.scopus.com/inward/record.url?scp=85132396021&partnerID=8YFLogxK

U2 - 10.1080/13647830.2022.2083525

DO - 10.1080/13647830.2022.2083525

M3 - Article

AN - SCOPUS:85132396021

VL - 26.2022

SP - 896

EP - 915

JO - Combustion theory and modelling

JF - Combustion theory and modelling

SN - 1364-7830

IS - 5

ER -