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

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Chapter 2<br />

fundamental processes such as ignition, NO, and soot formation, and f<strong>la</strong>me quenching.<br />

Moreover, some turbulent f<strong>la</strong>me mo<strong>de</strong>ls prescribe the turbulent burning velocity as a<br />

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

<strong>de</strong>pen<strong>de</strong>nce of the <strong>la</strong>minar burning velocity, f<strong>la</strong>me thickness, ignition temperature, heat<br />

release rate and f<strong>la</strong>me quenching on various system parameters can be a valuable<br />

diagnostic and <strong>de</strong>sign aid.<br />

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

There is a significant discrepancy in measuring burning velocities, which gives an<br />

indication of the difficulties and uncertainties associated with experimental<br />

<strong>de</strong>termination of f<strong>la</strong>me properties. In the light of the earlier experimental studies of<br />

Markstein, (1964), the asymptotic analysis of Klimov, (1963), and the computations of<br />

<strong>la</strong>minar f<strong>la</strong>me structure with <strong>de</strong>tailed chemical kinetics by several researchers, all of<br />

which show the importance of the f<strong>la</strong>me stretch rate (Dixon-Lewis, 1991). There can be<br />

little doubt that this is often neglected key variable (Law, 1989). It follows that any<br />

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

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

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

by the value of the appropriated Markstein length.<br />

For these reasons this chapter begins with the <strong>de</strong>finition of stretch rate and the<br />

corresponding Karlovitz and Markstein numbers. Following, the theory evolved with the<br />

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

and constant pressure methods due to be extensively used. This part of the chapter<br />

ends with the f<strong>la</strong>mmability limits <strong>de</strong>scription as is another important parameter of<br />

premixed <strong>la</strong>minar f<strong>la</strong>mes.<br />

2.5.1 F<strong>la</strong>me stretch<br />

A f<strong>la</strong>me surface propagating in a uniform flow field is submitted to strain and curvature<br />

effects leading to changes in the frontal area. Karlovitz et al., (1953) and Markstein,<br />

(1964) initiated the study of stretched premixed f<strong>la</strong>mes and <strong>de</strong>monstrated the<br />

importance of the aerodynamic stretching and the preferential diffusion on the f<strong>la</strong>me<br />

response in terms of f<strong>la</strong>me front instability.<br />

The f<strong>la</strong>me stretch factor (κ) is <strong>de</strong>fined as the re<strong>la</strong>tive rate of change of f<strong>la</strong>me surface<br />

area (A) (Williams, 1985):<br />

41

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