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Untitled - Aerobib - Universidad Politécnica de Madrid

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Chapter 6<br />

Laminar flames<br />

6.1 Introduction<br />

It was <strong>de</strong>monstrated in chapter 4 that through a combustible mixture of gases two<br />

types of combustion waves may propagate: <strong>de</strong>tonation waves and <strong>de</strong>flagration waves<br />

or flames. Chapter 5 inclu<strong>de</strong>s the analysis of the nature of such waves, their structure<br />

and the conditions which <strong>de</strong>termine their propagation velocity. This analysis proved<br />

that while in <strong>de</strong>tonation waves the propagation velocity is <strong>de</strong>termined only by a condition<br />

of mechanical stability within the zone of burnt gases, which simplifies extremely<br />

its <strong>de</strong>termination, when <strong>de</strong>aling with flames their propagation velocity is <strong>de</strong>termined<br />

by an internal equilibrium between the processes of chemical reaction, heat transfer<br />

(conductivity) and transport of the chemical species (diffusion), which makes the<br />

study specially difficult.<br />

The initial attempt to establish a theory on these bases, and in particular the<br />

<strong>de</strong>duction of the first formula for the computation of the propagation velocity of a<br />

flame through a given mixture, which is the fundamental problem of combustion, is<br />

own to Mallard and Le Chatelier [1]. Their theory is purely thermal and it establishes<br />

a primitive balance between the heat received by the gases through conduction, when<br />

an assumed ignition temperature is reached, and the heat content of these gases. The<br />

concept of reaction velocity is not applied in this theory.<br />

The work by Mallard and Le Chatelier was the starting point for the <strong>de</strong>velopment<br />

of the “thermal theories of the flame”, so called because they did not inclu<strong>de</strong> the<br />

diffusion of species.<br />

The i<strong>de</strong>a of chemical reaction velocity, incorporated by Crussard [2] to this<br />

thermal mo<strong>de</strong>l, was a <strong>de</strong>finite step forward in the progress of the theory. From there<br />

131

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