TY - GEN
T1 - Investigation of turbulence–flame interaction using the Schur decomposition
AU - Erraiy, A.
AU - Boukharfane, R.
AU - Perez, Francisco E.Hernández
AU - Im, Hong G.
AU - Parsani, M.
N1 - Funding Information:
The research work was sponsored by King Abdullah University of Science and Technology (KAUST) and made use of the computer clusters at KAUST Supercomputing Laboratory (KSL) and the Supercomputing Laboratory and the Extreme Computing Research Centre.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2022
Y1 - 2022
N2 - In the framework of turbulence-flame interaction, the flame is characterized by the gradient of a reactive scalar such as the progress variable, whereas the turbulence is represented by the vorticity and the strain rate. Quantitative assessment of this interaction is performed trough the study of the coupled transport between these quantities that are subject to the effects of heat release and chemical reactions. The present analysis aims at improving the understanding of the small scale turbulence – flame interaction properties, through the introduction of an additive decomposition of the strain rate and vorticity fields into their local and non-local components. Such a decomposition presents the advantage of dissociating the local dynamics, which are associated to the eigenvalues, from the asymmetric effects induced by the contribution of the deviatoric part of the pressure Hessian and viscous mechanisms. The respective role of the local and non-local effects is studied for a broad range of Karlovitz numbers, by virtue of direct numerical simulations (DNS) of turbulent, premixed, lean, and statistically planar flames of methane-air.
AB - In the framework of turbulence-flame interaction, the flame is characterized by the gradient of a reactive scalar such as the progress variable, whereas the turbulence is represented by the vorticity and the strain rate. Quantitative assessment of this interaction is performed trough the study of the coupled transport between these quantities that are subject to the effects of heat release and chemical reactions. The present analysis aims at improving the understanding of the small scale turbulence – flame interaction properties, through the introduction of an additive decomposition of the strain rate and vorticity fields into their local and non-local components. Such a decomposition presents the advantage of dissociating the local dynamics, which are associated to the eigenvalues, from the asymmetric effects induced by the contribution of the deviatoric part of the pressure Hessian and viscous mechanisms. The respective role of the local and non-local effects is studied for a broad range of Karlovitz numbers, by virtue of direct numerical simulations (DNS) of turbulent, premixed, lean, and statistically planar flames of methane-air.
UR - http://www.scopus.com/inward/record.url?scp=85123573686&partnerID=8YFLogxK
U2 - 10.2514/6.2022-1740
DO - 10.2514/6.2022-1740
M3 - Conference contribution
AN - SCOPUS:85123573686
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -