A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction

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A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction. / Tomasch, Stefanie; Swaminathan, Nedunchezhian; Spijker, Christoph et al.
In: Combustion Science and Technology, Vol. ??? Stand: 9. Dezember 2024, No. ??? Stand: 9. Dezember 2024, 2023.

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Tomasch S, Swaminathan N, Spijker C, Ertesvåg IS. A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction. Combustion Science and Technology. 2023;??? Stand: 9. Dezember 2024(??? Stand: 9. Dezember 2024). doi: 10.1080/00102202.2023.2239466

Author

Tomasch, Stefanie ; Swaminathan, Nedunchezhian ; Spijker, Christoph et al. / A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction. In: Combustion Science and Technology. 2023 ; Vol. ??? Stand: 9. Dezember 2024, No. ??? Stand: 9. Dezember 2024.

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@article{9e68b5386f4c442786682fc76117b0b9,
title = "A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction",
abstract = "Large Eddy Simulations (LES) of turbulent lean-premixed flames of V- and M-shape are presented. A simple algebraic closure with the ability to capture finite-rate chemistry effects is used for subgrid reaction rate modeling. The V-shaped flame is stabilized in the inner shear layer between a swirling annular jet and a central recirculating bubble in a sudden expansion duct. The M-shaped flame is stabilized in the inner and outer shear layer, adjoining the corner recirculation zone induced by the vertical step. The focus of the study is on the flow fields and shapes of the flames, which distinguish themselves through different heat load and sensitivity to local extinction. Good agreement with measurements is observed for the cold and the reacting flow cases. The numerical results suggest that the entrainment of hot gases into the outer recirculation zone occurs close to the impingement point of the swirling annular jet on the wall and this process is strongly dependent on intense vortical structures in the outer shear layer. The results further suggest that local extinction influences the position of the flame in the inner shear layer and, thereby, also the intensity of the local entrainment process.",
keywords = "dissipation, Lean premixed combustion, LES, OpenFOAM, progress variable reaction rate",
author = "Stefanie Tomasch and Nedunchezhian Swaminathan and Christoph Spijker and Ertesv{\aa}g, {Ivar S.}",
note = "Publisher Copyright: {\textcopyright} 2023 The Author(s). Published with license by Taylor & Francis Group, LLC.",
year = "2023",
doi = "10.1080/00102202.2023.2239466",
language = "English",
volume = "??? Stand: 9. Dezember 2024",
journal = "Combustion Science and Technology",
issn = "1563-521X ",
number = "??? Stand: 9. Dezember 2024",

}

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TY - JOUR

T1 - A Numerical Study of Flow Structures and Flame Shape Transition in Swirl-Stabilized Turbulent Premixed Flames Subject to Local Extinction

AU - Tomasch, Stefanie

AU - Swaminathan, Nedunchezhian

AU - Spijker, Christoph

AU - Ertesvåg, Ivar S.

N1 - Publisher Copyright: © 2023 The Author(s). Published with license by Taylor & Francis Group, LLC.

PY - 2023

Y1 - 2023

N2 - Large Eddy Simulations (LES) of turbulent lean-premixed flames of V- and M-shape are presented. A simple algebraic closure with the ability to capture finite-rate chemistry effects is used for subgrid reaction rate modeling. The V-shaped flame is stabilized in the inner shear layer between a swirling annular jet and a central recirculating bubble in a sudden expansion duct. The M-shaped flame is stabilized in the inner and outer shear layer, adjoining the corner recirculation zone induced by the vertical step. The focus of the study is on the flow fields and shapes of the flames, which distinguish themselves through different heat load and sensitivity to local extinction. Good agreement with measurements is observed for the cold and the reacting flow cases. The numerical results suggest that the entrainment of hot gases into the outer recirculation zone occurs close to the impingement point of the swirling annular jet on the wall and this process is strongly dependent on intense vortical structures in the outer shear layer. The results further suggest that local extinction influences the position of the flame in the inner shear layer and, thereby, also the intensity of the local entrainment process.

AB - Large Eddy Simulations (LES) of turbulent lean-premixed flames of V- and M-shape are presented. A simple algebraic closure with the ability to capture finite-rate chemistry effects is used for subgrid reaction rate modeling. The V-shaped flame is stabilized in the inner shear layer between a swirling annular jet and a central recirculating bubble in a sudden expansion duct. The M-shaped flame is stabilized in the inner and outer shear layer, adjoining the corner recirculation zone induced by the vertical step. The focus of the study is on the flow fields and shapes of the flames, which distinguish themselves through different heat load and sensitivity to local extinction. Good agreement with measurements is observed for the cold and the reacting flow cases. The numerical results suggest that the entrainment of hot gases into the outer recirculation zone occurs close to the impingement point of the swirling annular jet on the wall and this process is strongly dependent on intense vortical structures in the outer shear layer. The results further suggest that local extinction influences the position of the flame in the inner shear layer and, thereby, also the intensity of the local entrainment process.

KW - dissipation

KW - Lean premixed combustion

KW - LES

KW - OpenFOAM

KW - progress variable reaction rate

UR - http://www.scopus.com/inward/record.url?scp=85166935490&partnerID=8YFLogxK

U2 - 10.1080/00102202.2023.2239466

DO - 10.1080/00102202.2023.2239466

M3 - Article

VL - ??? Stand: 9. Dezember 2024

JO - Combustion Science and Technology

JF - Combustion Science and Technology

SN - 1563-521X

IS - ??? Stand: 9. Dezember 2024

ER -