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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 />

In or<strong>de</strong>r to quantify the thermal losses of different mixtures special care must be taken<br />

in the heat flux integration. The integration time should capture the entire phenomenon.<br />

The cooling time is possible to control by establishing a certain cooling period.<br />

However, the <strong>combustion</strong> time changes with the fuel, initial pressure and equivalence<br />

ratio, which calcu<strong>la</strong>tion is not straightforward. Therefore, the comparison of heat flux<br />

estimative already shown in figures 4.41-4.49 is ma<strong>de</strong> based on the heat flux peaks<br />

(Table 4.4).<br />

Table 4.4 – Heat Flux peaks for stoichiometric syngas-air and methane-air mixtures.<br />

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

Qw (kW/m 2 ) Updraft Downdraft Methane (Boust, 2006)<br />

1.0 bar, φ=0.8 216 kW/m 2 350 kW/m 2 -<br />

1.0 bar, φ=1.0 368 kW/m 2 402 kW/m 2 649 kW/m 2<br />

1.0 bar, φ=1.2 220 kW/m 2 313 kW/m 2 -<br />

5.0 bar, φ=1.0 777 kW/m 2 949 kW/m 2 (*) 1622 kW/m 2<br />

(*) linear interpo<strong>la</strong>tion.<br />

From Table 4.4 some conclusions can be drawn:<br />

- The heat flux increases with initial pressure increase for all cases. The amount<br />

(volume and energy) of the explosive mixture insi<strong>de</strong> the vessel increases with<br />

initial pressure increase.<br />

- The heat flux increases with the heat value of the fuel-air mixture. In this case,<br />

one should also take into account the air-fuel ratio.<br />

- The equivalence ratio has the influence of <strong>de</strong>creasing the heat flux compared to<br />

stoichiometric mixtures and follows the behavior of pressure peak.<br />

The thickness of wall quench <strong>la</strong>yers is a primary source of unburned fuels (Saeed and<br />

Stone, 2004). Thus, this <strong>combustion</strong> characteristic is very important and was predicted<br />

for stoichiometric updraft and downdraft syngas compositions by the Westbrook<br />

criterion <strong>de</strong>fined by a zero f<strong>la</strong>me stretch (figure 4.51). This is practically the case when<br />

the f<strong>la</strong>me reaches the wall given the <strong>la</strong>rge curvature radius. The Westbrook criterion is<br />

valid in pressure range 1-40 bar and burning velocity corre<strong>la</strong>tion used in the co<strong>de</strong><br />

shows to be valid up to 33 bar, thus one impose this limit to quenching distance<br />

estimation.<br />

136

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