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Untitled - Aerobib - Universidad Politécnica de Madrid

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274 CHAPTER 11. SIMILARITY IN COMBUSTION. APPLICATIONS<br />

11.5 Flame stabilization<br />

In the preceding chapter we have studied the aerodynamic field of a flow with a flame<br />

stabilized by a hol<strong>de</strong>r. We verified that the expansion of the burnt gases may originate<br />

a chocking effect which imposses a limitation to the maximum velocity of the flow<br />

entering the chamber.<br />

Another limitation to this velocity, bearing a great practical interest, is that impossed<br />

by the need to fix the flame to the hol<strong>de</strong>r in or<strong>de</strong>r to maintain combustion.<br />

In fact, it has been experimentally observed that when the velocity of the incoming<br />

flow exceeds a certain value, the flame blows out. The blowing velocity of the flame<br />

is <strong>de</strong>termined by the composition and state of the combustible mixture and by the<br />

characteristics of the hol<strong>de</strong>r. The problem arising from this circunstance holds a great<br />

practical interest in the new propulsion systems, specially in ramjets and after-burners,<br />

in which their limits of practical application are often <strong>de</strong>termined by this effect. Consequently,<br />

this phenomenon has been the subject of a particular interest during the last<br />

years and abundant experimental data have been gathered on a great variety of types of<br />

hol<strong>de</strong>r and on the influence of the parameters of the mixture on the blowing velocity<br />

of the flame. An extensive bibliography on the matter can be found in the proceedings<br />

of the congresses and colloquia on combustion celebrated in recent years.<br />

The initial study on this problem was carried out by Scurlock [16], who pointed<br />

out the significance of the recirculation zone that forms in the wake of the hol<strong>de</strong>r. Figure<br />

11.2 taken from Ref. [17] illustrates the phenomenon. Behind the hol<strong>de</strong>r a recirculation<br />

zone forms in which the flame stabilizes. The boundary of this zone consists<br />

in a mixing zone formed by a free boundary layer which separates the unburnt gases<br />

from the combustion products. Within this mixing zone is where the combustible<br />

gases ignite through a process of heat and mass transport, whose characteristics are<br />

not yet well known.<br />

Since the presence of a recirculation zone is essential for the existence of the<br />

flame, the hol<strong>de</strong>rs used for this purpose are given a shape which produces a large<br />

aerodynamic wake.<br />

In many of the tests conducted, attempts were ma<strong>de</strong> to establish a correlation<br />

between the blowing velocity of the flame, in a mixture of given composition and<br />

temperature, and the size of the hol<strong>de</strong>r, characterized by a linear dimension of the<br />

same, for example by its diameter in the case of a hol<strong>de</strong>r of circular section as the one<br />

shown in Fig. 11.2. A summary of the works performed from this stand-point, up to<br />

1953, and of the state or knowledge at the time may be found in Ref. [18].

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