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Journal ArticleDOI

Flame Propagation in a Tube: The Legacy of Henri Guenoche

Derek Bradley
- 01 Sep 2000 - 
- Vol. 158, Iss: 1, pp 15-33
TLDR
In this paper, the effects of flame stretch on the laminar burning velocity of a tube are discussed. And the effect of the Karlovitz stretch factor on the burn rate is discussed.
Abstract
Since the time of Mallard and Le Chatelier there has been a fascination with the problems of flame propagation in tubes. An important goal has been the development of a reliable technique to measure accurately the most basic combustion parameter, the laminar burning velocity. On the one hand a stable, steady-state, flame is necessary to do this, while on the other hand many flames are inherently unstable. These conflicting tendencies have been the source of much creative combustion thinking, not least from Guenoche. The paper attempts to indicate how his work has contributed to our present appreciation of the effects of flame stretch, thermo-diffusion, Darrieus – Landau and Taylor instabilities. Some practical consequences of the effects of these on the burn rate are briefly discussed. Laminar burning velocity and its measurement The purpose of the present paper is to show how Henri Guenoche’s painstaking descriptions and analyses of experimental findings concerning flame propagation in tubes contribute greatly to our current fundamental understanding of combustion. In 1883 Mallard and Le Chatelier [1] showed that the condition of a tube closed at one end with ignition at the other, open, end is probably the one best able to achieve a constant flame speed over a distance sufficient for the measurement of the laminar burning velocity. Thereafter, the flame oscillates, particularly with lean CH4 and H2 and rich hydrocarbon mixtures with air, and then assumes a cellular structure with an enhanced flame speed [2]. Their painstaking studies of the factors that give rise to a regime in which the flame speed is constant led Guenoche and Laffitte [3] to suppress any tendencies to acoustic oscillations by fitting an orifice to vent the burned gas at the open end of the tube, a practice adopted by subsequent workers, to make the vertical tube method a recommended one for measuring burning velocity [4]. Conversely, in the unstable regime forcing oscillations can induce a cellular structure [5]. When the flame attains a constant flame speed through the use of orifice damping its shape hardly changes and hence the effects of flame stretch rate are minimal. In the last decade the quantitative understanding of these effects stretch has advanced considerably and it is now almost mandatory to measure stretch-free values of burning velocity, λ u , together with values of Markstein numbers, Ma, to express the effects of flame stretch rate, in conjunction with the Karlovitz stretch factor, K. Flame stretch can either increase or decrease the burning velocity to a value,

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Citations
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Journal ArticleDOI

Turbulent burning velocity, burned gas distribution, and associated flame surface definition

TL;DR: In this paper, an experimental study of premixed, turbulent, gaseous explosion flames in a fan-stirred bomb is reported, and various definitions are scrutinized and different flame radii presented, along with the associated turbulent burning velocities.
Journal ArticleDOI

Premixed flamelet modelling: Factors influencing the turbulent heat release rate source term and the turbulent burning velocity

TL;DR: In this paper, a flamelet approach is adopted in a study of the factors affecting the volumetric heat release source term in turbulent combustion, which is expressed as the product of an instability enhanced burning rate factor.
Journal ArticleDOI

Darrieus–landau and thermo-acoustic instabilities in closed vessel explosions

TL;DR: In this paper, a spherical explosion bomb was used to investigate the effect of Rayleigh-Taylor instabilities on the flame speed and the structure of high pressure flames using dual wall ignitions.
Journal ArticleDOI

The turbulent burning velocity of iso-octane/air mixtures

TL;DR: In this paper, high speed schlieren images were used to derive turbulent burning velocities of iso-octane air mixtures, and the results obtained in this study have been compared with those evaluated for a number turbulent burning velocity correlations and the differences are discussed.
Journal ArticleDOI

Experimental characterization of burning velocities of premixed methane-air and hydrogen-air mixtures in a constant volume combustion bomb at moderate pressure and temperature

TL;DR: In this paper, a two-zone combustion model is used to analyse the experimental pressure trace and compute the thermodynamic variables that cannot be directly measured, with the mass burning rate and the associated burning velocity as the model results.
References
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Journal ArticleDOI

Laminar burning velocity and Markstein lengths of methane–air mixtures

TL;DR: In this article, the effect of temperature on the mass burning rate of a spherically expanding flame propagating at constant pressure and the effect by the associated Markstein lengths was investigated.
Journal ArticleDOI

The measurement of laminar burning velocities and Markstein numbers for iso-octane-air and iso-octane-n-heptane-air mixtures at elevated temperatures and pressures in an explosion bomb

TL;DR: In this article, the effects of the initial mixture temperature and pressure on these parameters also have been examined and data have been obtained for iso-octane-air mixtures at initial temperatures between 358 K and 450 K, at pressures between 1 and 10 bar, and equivalence ratios, φ, of 0.8 and 1.0.
Book

Nonsteady flame propagation

H. Markstein
Journal ArticleDOI

Burning Velocities, Markstein Lengths, and Flame Quenching for Spherical Methane-Air Flames: A Computational Study

TL;DR: In this paper, the reduced kinetic, C1, scheme of Mauss and Peters is employed for a range of equivalence ratios under atmospheric conditions, with flame propagation at constant pressure.
Journal ArticleDOI

Direct experimental determination of laminar flame speeds

TL;DR: In this paper, a new methodology is proposed for direct experimental determination of laminar flame speeds, which includes the use of the stagnation flow configuration and large separation distances betwenn the nozzle and the stagnation plane, which allow for the establishment of Bunsen-type flames as the flow rate is reduced.
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