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Etude de la combustion de gaz de synthèse issus d'un processus de ...

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Experimental and numerical <strong>la</strong>minar syngas <strong>combustion</strong><br />

across the f<strong>la</strong>me, increasing with increasing <strong>de</strong>nsity ratio, σ. Thus σ is probably the<br />

most sensitive parameter controlling the onset of hydrodynamic instability. Next to σ,<br />

the f<strong>la</strong>me thickness, δ, is also expected to have a strong influence on the hydrodynamic<br />

instability, for two reasons. First, it measures the influence of curvature which, being<br />

positive for the outwardly propagating spherical f<strong>la</strong>me, has a stabilizing effect on the<br />

cellu<strong>la</strong>r <strong>de</strong>velopment. The thinner the f<strong>la</strong>me, the weaker is the influence of curvature<br />

and consequently the stronger is the <strong>de</strong>stabilizing propensity. The second influence is<br />

that it controls the intensity of the baroclinic torque <strong>de</strong>veloped over a slightly wrinkled<br />

f<strong>la</strong>me surface, which <strong>de</strong>pends on the <strong>de</strong>nsity gradient across the f<strong>la</strong>me and the<br />

pressure gradient along the f<strong>la</strong>me (Sun et al., 1999).<br />

tel-00623090, version 1 - 13 Sep 2011<br />

For the <strong>de</strong>velopment of the diffusional-thermal instability, an appropriate parameter<br />

representing the effect of non-equidiffusion is the f<strong>la</strong>me Lewis number, L e [Markstein,<br />

(1951); Matalon and Matkowsky, (1982); Law and Sung, (2000)]. It is well established<br />

and un<strong>de</strong>rstood theoretically that unstretched f<strong>la</strong>mes are diffusionally unstable (stable)<br />

for L e that are smaller (greater) than a value slightly less than unity. However, the<br />

calcu<strong>la</strong>tion of effective Lewis number for a multi-component fuel mixture is not as<br />

straightforward as for pure fuel-air mixtures and is a subject that is out of the scope of<br />

the present work.<br />

4.1.1.2 F<strong>la</strong>me Radius<br />

Fig. 4.16 gives the variations of f<strong>la</strong>me radius versus the time for syngas-air mixtures.<br />

The study shows that f<strong>la</strong>me expands spherically after the ignition, and the f<strong>la</strong>me radius<br />

will increase rapidly in the subsequent process. There are a quasi-linear corre<strong>la</strong>tion<br />

between f<strong>la</strong>me radius and time for all syngas cases. The higher gradient of radius-time<br />

curves is obtained for stoichiometric syngas-air mixtures. The lean (φ=0.8) and rich<br />

(φ=1.2) syngas-air mixtures have simi<strong>la</strong>r gradients in the updraft case. This difference<br />

increases for the downdraft syngas case. Fluidized syngas has the lowest radius-time<br />

curve gradients. Information for rich mixture of fluidized syngas is missing due to<br />

ignition difficulties.<br />

According to the Markstein view the gradient of the radius-time curve reflects the<br />

stretching effectiveness of f<strong>la</strong>me. For an unstable f<strong>la</strong>me, the gradient of the radius-time<br />

curve will <strong>de</strong>crease with the f<strong>la</strong>me expansion, while for a stable f<strong>la</strong>me; the gradient of<br />

the radius-time curve will increase with the f<strong>la</strong>me expansion. The quasi-linear<br />

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