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

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Chapter 4<br />

0.5<br />

0.4<br />

φ =1.0<br />

Su (m/s)<br />

0.3<br />

0.2<br />

Updraft<br />

Dow ndraf t<br />

0.1<br />

Fluidized<br />

0.0<br />

0 100 200 300 400 500 600<br />

κ (s -1 )<br />

0.5<br />

φ=1.2<br />

0.4<br />

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

Su (m/s)<br />

0.3<br />

0.2<br />

0.1<br />

0.0<br />

Updraft<br />

Downdraft<br />

0 100 200 300 400 500 600 700<br />

κ (s -1 )<br />

Figure 4.18b – Stretched burning velocity versus stretch rate for syngas-air mixtures at various<br />

equivalence ratios.<br />

The unstretched <strong>la</strong>minar burning velocity, S , shown in Fig. 4.19 is <strong>de</strong>rived from the<br />

value of the unstretched f<strong>la</strong>me speed and the expansion factor which is evaluated<br />

using the adiabatic f<strong>la</strong>me calcu<strong>la</strong>tion via the Gaseq co<strong>de</strong> package, which can be found<br />

in the Appendix B.<br />

0<br />

u<br />

S 0 u (m/s)<br />

0.4<br />

0.3<br />

0.2<br />

Updraft<br />

Dow ndraft<br />

Fluidized<br />

0.1<br />

0<br />

0.6 0.8 1 1.2<br />

Equivalence ratio<br />

Figure 4.19- Unstretched f<strong>la</strong>me speed versus equivalence ratio of syngas-air mixtures.<br />

105

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