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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.6. EXAMPLE 141<br />

generally impossible to obtain explicit solutions for the equations. Hence, it is necessary<br />

to resort to cumbersome numerical integrations or to analytical methods which<br />

will be discussed further on. However, in or<strong>de</strong>r to illustrate the nature of the solutions<br />

and the way in which the eigenvalue appears <strong>de</strong>termined, the present paragraph offers<br />

an example in which through an a<strong>de</strong>quate simplification of both transport coefficients<br />

and chemical reaction velocity, it is possible to obtain an explicit solution of the problem<br />

giving correct qualitative predictions. A possible objection to this solution could<br />

be that the results obtained <strong>de</strong>pend on the ignition temperature of the mixture, which,<br />

as before said, does not exist. But this is due to the fact that the simplification assumed<br />

for the reaction velocity is excessive and consequently the inconvenient will vanish for<br />

more realistic cases, as will be proven in the following.<br />

For this example the following assumptions will be adopted:<br />

1) The coefficient of thermal conductivity λ and the product ρD are constant.<br />

2) The reaction is of first-or<strong>de</strong>r and its velocity is in<strong>de</strong>pen<strong>de</strong>nt from temperature, in<br />

which case it has the form 1 w = ρ 0 k(1 − Y ). (6.23)<br />

It is precisely this simplified form of the reaction velocity and, in special, the fact<br />

that in it the activation energy is assumed to be zero, an indispensable condition<br />

for the integrability of the system, which makes the solution <strong>de</strong>pends on the<br />

ignition temperature, as aforesaid.<br />

When expression (6.23) is taken into (6.2), it gives<br />

The diffusion equation subsists in the form (6.3)<br />

m dε<br />

dx = ρ 0k(1 − Y ). (6.24)<br />

ρD dY<br />

dx<br />

= m(Y − ε). (6.25)<br />

Finally, when the dimensionless temperature θ = T/T f is introduced, the energy<br />

equation (6.5.a) may be written<br />

where is θ 0 = T 0 /T f .<br />

λ dθ<br />

mc p dx = θ − 1 + (1 − θ 0)(1 − ε), (6.26)<br />

1 See §8 of Chap. 1.

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