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Effects of Lewis number, density ratio and gravity on burning velocity and conditional statistics in stagnating turbulent premixed flames SCIE SCOPUS

Title
Effects of Lewis number, density ratio and gravity on burning velocity and conditional statistics in stagnating turbulent premixed flames
Authors
Kwon, JHuh, KY
Date Issued
2014-09-03
Publisher
TAYLOR & FRANCIS LTD
Abstract
DNS is performed to analyse the effects of Lewis number (Le), density ratio and gravity in stagnating turbulent premixed flames. The results show good agreement with those of Lee and Huh (Combustion and Flame, Vol. 159, 2012, pp. 1576-1591) with respect to the turbulent burning velocity, S-T, in terms of turbulent diffusivity, flamelet thickness, mean curvature and displacement speed at the leading edge. In all four stagnating flames studied, a mean tangential strain rate resulting in a mean flamelet thickness smaller than the unstretched laminar flame thickness leads to an increase in S-T. A flame cusp of positive curvature involves a superadiabatic burned gas temperature due to diffusive-thermal instability for an Le less than unity. Wrinkling tends to be suppressed at a larger density ratio, not enhanced by hydrodynamic instability, in the stagnating flow configuration. Turbulence is produced, resulting in highly anisotropic turbulence with heavier unburned gas accelerating through a flame brush by Rayleigh-Taylor instability. Results are also provided on brush thickness, flame surface density and conditional velocities in burned and unburned gas and on flame surfaces to represent the internal brush structures for all four test flames.
Keywords
turbulent burning velocity; diffusive-thermal instability; hydrodynamic instability; Rayleigh-Taylor instability; conditional average; COMBUSTION; SCALE
URI
https://oasis.postech.ac.kr/handle/2014.oak/14033
DOI
10.1080/13647830.2014.930513
ISSN
1364-7830
Article Type
Article
Citation
COMBUSTION THEORY AND MODELLING, vol. 18, no. 4-5, page. 501 - 514, 2014-09-03
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허강열HUH, KANG YUL
Dept of Mechanical Enginrg
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