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image/svg+xml Jakob Voss, based on art designer at PLoS, modified by Wikipedia users Nina and Beao Closed Access logo, derived from PLoS Open Access logo. This version with transparent background. http://commons.wikimedia.org/wiki/File:Closed_Access_logo_transparent.svg Jakob Voss, based on art designer at PLoS, modified by Wikipedia users Nina and Beao Proceedings of the C...arrow_drop_down
image/svg+xml Jakob Voss, based on art designer at PLoS, modified by Wikipedia users Nina and Beao Closed Access logo, derived from PLoS Open Access logo. This version with transparent background. http://commons.wikimedia.org/wiki/File:Closed_Access_logo_transparent.svg Jakob Voss, based on art designer at PLoS, modified by Wikipedia users Nina and Beao
Proceedings of the Combustion Institute
Article . 2011 . Peer-reviewed
License: Elsevier TDM
Data sources: Crossref
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On interaction of centrally-ignited, outwardly-propagating premixed flames with fully-developed isotropic turbulence at elevated pressure

Authors: C.C. Liu; S.S. Shy; H.C. Chen; M.W. Peng;

On interaction of centrally-ignited, outwardly-propagating premixed flames with fully-developed isotropic turbulence at elevated pressure

Abstract

Abstract A new apparatus for the study of turbulent premixed flames at atmospheric and elevated pressures is proposed. The apparatus includes a high-pressure fan-stirred cruciform burner, the inner chamber, which is resided in a relatively large pressure-absorbing safety chamber (the outer chamber). Both chambers are optically accessible, allowing direct visualization and measurement of flame and turbulence interactions. The inner burner applies the same turbulence generating mechanism as that previously reported by Shy et al. [10] , capable of generating intense near-isotropic turbulence. The additional modification lies in its vertical vessel which has four sensitive pressure-releasing valves installed symmetrically, so that the pressure difference between the inner and outer chambers during explosion can be eliminated. Flame speed measurements for centrally-ignited, outwardly-propagating lean CH 4 –air flames at the equivalence ratio ϕ = 0.8 under both quiescent and turbulent conditions are conducted over an initial pressure range of p = 0.1–1 MPa. It is found that, contrary to the popular scenario for laminar flames, the coupling influence of elevated pressure and turbulence significantly enhances turbulent flame speeds. Our experimental data show that the unstretched laminar burning velocities ( S L ) decrease with p −0.52 , while turbulent burning velocities ( S T ) increase with p 0.14 when a constant turbulent fluctuating velocity u′ ≈ 1.4 m/s is applied. In terms of the power law relation proposed by Kobayashi and his co-workers, we found that S T / S L ≈ 1.07[( u′ / S L )( p / p 0 )] 0.44 where p 0 is the atmospheric pressure, showing a similar increasing trend but with much lower values of S T / S L to what they found in a Bunsen-type burner. It is suggested that S T ∼ p 0.14 is attributed to further flame surface area increment induced by the enhancement of hydrodynamic instability due to the decrease of kinematic viscosity at elevated pressure.

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selected citations
These citations are derived from selected sources.
This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Citations provided by BIP!
popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
BIP!Popularity provided by BIP!
influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
BIP!Influence provided by BIP!
impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
BIP!Impulse provided by BIP!
40
Top 10%
Top 10%
Top 10%
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