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Untitled - Aerobib - Universidad Politécnica de Madrid

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136 CHAPTER 6. LAMINAR FLAMES<br />

which, furthermore, enables (6.5) to be written as<br />

λ dT<br />

dx = mc (<br />

p (T − Tf ) + (T f − T 0 )(1 − ε) ) , (6.5.a)<br />

in which form it will be used further on.<br />

As for the second condition (6.9) it is also satisfied for x = +∞, since the<br />

condition of chemical equilibrium for the products may be expressed as<br />

w(1, ρ f , T f ) = 0. (6.11)<br />

To the contrary, condition dε → 0 for x → −∞, will not be satisfied unless<br />

dx<br />

w(0, ρ 0 , T 0 ) = 0, (6.12)<br />

which, generally, will be in contradiction with the laws of Chemical Kinetics.<br />

This circumstance implies a fundamental difficulty, whose origin lies upon the<br />

fact that it is impossible to maintain invariable the composition of the unburnt gases<br />

located before the wave, as imposed by boundary conditions (6.7) and (6.9), when the<br />

reaction velocity of such gases is not zero.<br />

The existence of stationary combustion waves observed in practice may be<br />

explained by the fact that such waves do not correspond exactly to the one-dimensional<br />

mo<strong>de</strong>l proposed in this work, since the mixing of reactant species forms, in general,<br />

shortly before they reach the wave, which always looses a certain amount of heat<br />

through the walls of the flame hol<strong>de</strong>r, for example, through the walls of the burner.<br />

Furthermore, these walls act as chain breakers for the chemical reactions of the wave.<br />

There is a possibility of eluding the above mentioned difficulty by incorporating<br />

to the one-dimensional mo<strong>de</strong>l the effect of all these complex circumstances, which<br />

prevent the reaction of the unburnt gases in a real flame, through a slight modification<br />

of the boundary conditions at the neighborhood of the “cold limit” of the flame, which<br />

may be attained in several different ways. The practical interest of these solutions<br />

is based on the fact that for reactions with an appreciable activation energy, as those<br />

expected in combustion, the structure and propagation velocity of the flame are insensible<br />

to a modification of the said boundary conditions, which makes it unnecessary to<br />

<strong>de</strong>fine them exactly, within a wi<strong>de</strong> range of values of the <strong>de</strong>fining parameters. Moreover,<br />

the proposed solutions are equivalent since they lead to the same fundamental<br />

results. The following paragraph is <strong>de</strong>voted to a discussion of these solutions.

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