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Untitled - Aerobib - Universidad Politécnica de Madrid

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11.5. FLAME STABILIZATION 275<br />

Flame front<br />

End of recirculation zone<br />

Recirculation zone<br />

Flame hol<strong>de</strong>r<br />

Mixing zone<br />

Propagating zone<br />

Figure 11.2: Zones of a stabilized flame.<br />

The theoretical study of this problem is very difficult. Several theories are<br />

available whose <strong>de</strong>velopment may be found in the works listed un<strong>de</strong>r Refs. [19]<br />

through [21], but none of them has been experimentally confirmed. On the other<br />

hand, the correlation between experimental results as presented by Longwell is very<br />

difficult. At this stage it appears justified to perform the study by means of a dimensionless<br />

analysis, searching for the significant variables and the relation existing<br />

between them.<br />

Inasmuch as we are far from the actual regime in which the compressibility<br />

effect would appear, the dimensionless variable characteristic of the motion is the<br />

Reynolds number referred to the velocity and state of the gases before the hol<strong>de</strong>r and<br />

to a linear dimension of the same. The composition of the mixture is characterized by<br />

the relationship between the fuel fraction and that corresponding to the stoichiometric<br />

one. Finally, the variable we are trying to analyze is the blowing velocity or, if written<br />

in dimensionless form although it is not generally necesary, this velocity referred to<br />

the propagation velocity of the flame.<br />

Zukoski and Marble [22] have performed a very interesting systematic analysis<br />

on the experimental data available. A summary of this analysis appears in Figs. 11.3<br />

and 11.4<br />

Figure 11.3, corresponding to a circular flame hol<strong>de</strong>r as the one shown in<br />

Fig. 11.2, gives the following: a) the influence of the Reynolds number on the maximum<br />

blowing velocity of the flame, and b) the composition of the mixture for which<br />

such velocity is reached, for a given Reynolds number.<br />

Figure 11.4 shows the law of variation of the maximum blowing velocity as a<br />

function of the Reynolds number for a set of experiments performed by other authors<br />

with different types of flame hol<strong>de</strong>rs.

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