2005
DOI: 10.1016/j.pecs.2004.07.001
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Molecular transport effects on turbulent flame propagation and structure

A.N. Lipatnikov,
J. Chomiak
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Cited by 303 publications
(240 citation statements)
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“…This instability was investigated in a number of previous analyses. 30,55,[68][69][70][71][72] The linear stability analysis of thermo-diffusive instability for planar [33][34][35][36] and spherical 73,74 laminar premixed flames resulted in analytical expressions for the instability growth rate and largest wavenumber (smallest wavelength) of a perturbation that could trigger the instability. Interested readers are referred to Refs.…”
Section: Resultsmentioning
confidence: 99%
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“…This instability was investigated in a number of previous analyses. 30,55,[68][69][70][71][72] The linear stability analysis of thermo-diffusive instability for planar [33][34][35][36] and spherical 73,74 laminar premixed flames resulted in analytical expressions for the instability growth rate and largest wavenumber (smallest wavelength) of a perturbation that could trigger the instability. Interested readers are referred to Refs.…”
Section: Resultsmentioning
confidence: 99%
“…An alternative concept 54,55,69,80 of the Lewis number effects in premixed turbulent combustion emphasizes the propagation of highly stretched leading reaction zones into the unburned gas (the so-called leading edge concept). However, a comparison of the thermo-diffusive instability and leading point concepts is beyond the scope of the present study.…”
Section: Resultsmentioning
confidence: 99%
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“…In addition to the laminar burning velocity, flame stretch/species diffusion effects have been recognised as having a strong influence in premixed turbulent flames [23].…”
Section: Resultsmentioning
confidence: 99%
“…While the bending effect is well documented in experiments with premixed turbulent flames, as reviewed elsewhere [56,72], explanation and modeling of this effect is still the grand challenge to the combustion community.…”
Section: B Bending Effectmentioning
confidence: 99%