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

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Chapter 7<br />

composition on the condition of biomass used, the type of gasifier and conditions of<br />

pressure and temperature.<br />

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

Another issue evolved in this work is the <strong>combustion</strong>, which <strong>de</strong>tailed bibliographic<br />

revision allows to verify that in premixed f<strong>la</strong>mes, the <strong>la</strong>minar burning velocity and f<strong>la</strong>me<br />

structure data can be extremely useful in the analysis of fundamental processes such<br />

as ignition, NO, and soot formation, and f<strong>la</strong>me quenching. Also, turbulent f<strong>la</strong>me mo<strong>de</strong>ls<br />

often prescribe the turbulent burning velocity as a function of <strong>la</strong>minar burning velocity.<br />

Thus, <strong>de</strong>tailed information <strong>de</strong>scribing the <strong>de</strong>pen<strong>de</strong>nce of the <strong>la</strong>minar burning velocity,<br />

f<strong>la</strong>me thickness, ignition temperature, heat release rate and f<strong>la</strong>me quenching on<br />

various system parameters can be a valuable diagnostic and <strong>de</strong>sign aid. Burning<br />

velocity is a physicochemical constant for a given mixture. It is the velocity, re<strong>la</strong>tive of<br />

unburned gas, which a p<strong>la</strong>ne, one-dimensional f<strong>la</strong>me front travels along the normal to<br />

its surface. Clearly, it is the volume of combustible mixture, at its own temperature and<br />

pressure, consumed in unit time by unit area of f<strong>la</strong>me front. It is in<strong>de</strong>pen<strong>de</strong>nt of f<strong>la</strong>me<br />

geometry, burner size and flow rate. The experimental methods for burning velocity<br />

<strong>de</strong>termination are <strong>de</strong>scribed with emphasis for the constant volume and constant<br />

pressure methods. In the constant pressure method the <strong>la</strong>minar burning velocity and<br />

Markstein length are <strong>de</strong>duced from schlieren photographs. Moreover, any experimental<br />

or computed value of <strong>la</strong>minar burning velocity should be associated with a value of the<br />

f<strong>la</strong>me stretch rate. I<strong>de</strong>ally, the stretch-free value of the burning velocity should be<br />

quoted and the influence of stretch rate upon this value should be indicated by the<br />

value of the appropriated Markstein length. This is the main reason of the increasing<br />

use of the constant pressure method in which the stretch rate is clearly <strong>de</strong>fined. The<br />

main advantage of the constant volume method for <strong>de</strong>termining the burning velocity is<br />

the possibility of exploring a wi<strong>de</strong> range of pressures and temperatures with one<br />

explosion. This is the main reason of its utilization for burning velocity <strong>de</strong>termination in<br />

engine conditions.<br />

Following the biographic revision, the <strong>combustion</strong> characterization of typical syngas-air<br />

mixtures was initiated by the <strong>de</strong>termination of the f<strong>la</strong>mmability limits in spherical<br />

chamber. These results show that the pressure has a <strong>de</strong>finite effect on f<strong>la</strong>mmability<br />

limits of the syngas-air mixtures reducing the f<strong>la</strong>mmable region in the lean si<strong>de</strong>. The<br />

syngas <strong>combustion</strong> characterization continues with the <strong>la</strong>minar f<strong>la</strong>me characteristics to<br />

four equivalence ratios (0.6, 0.8, 1.0 and 1.2) within the f<strong>la</strong>mmability limits. The<br />

influence of stretch rate on f<strong>la</strong>me was <strong>de</strong>termined by the correspon<strong>de</strong>nt Markstein and<br />

Karlovitz numbers. Combustion <strong>de</strong>monstrates a linear re<strong>la</strong>tionship between f<strong>la</strong>me<br />

195

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