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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.11. IGNITION TEMPERATURE 161<br />

6.11 Ignition temperature<br />

We have established that, except when activation temperature θ a is zero or very small,<br />

the ignition temperature θ i bears no influence on the flame velocity unless it has a<br />

value close to the temperature of the burnt gases θ = 1, or very close to initial temperature<br />

θ 0 .<br />

1.6<br />

1.2<br />

θ a<br />

=0<br />

Λ −1/2<br />

0.8<br />

θ a<br />

=2<br />

0.4<br />

θ a<br />

=4<br />

θ a<br />

=8<br />

0.0<br />

0.0 0.2 0.4 0.6 0.8 1.0<br />

θ =0.125 0<br />

θ i<br />

Figure 6.14: Flame velocity as a function of the ignition temperature θ i for different values<br />

of the activation temperature θ a.<br />

This property is illustrated by Fig. 6.14, where the law of variation of Λ −1/2<br />

(to which u 0 is proportional as before said), as a function of θ i is shown for a typical<br />

case, corresponding to a first-or<strong>de</strong>r reaction, with a Lewis-Semenov number equal to<br />

unity and a temperature of the unburnt gases θ 0 = 0.125. The figure represents the<br />

solutions corresponding to values of θ a comprised between 0 and 8 and it is seen that<br />

except for the first case (θ a = 0), there exists a wi<strong>de</strong> range on values of θ i in which<br />

Λ −1/2 is practically constant, as it was previously announced. 7<br />

This property is of a general nature and it justifies the assumption of a ignition<br />

temperature which eliminate the difficulty of the cold boundary.<br />

7 For θ a ≫ 1 and θ i very close to θ 0 , it can be shown by means of asymptotic techniques that Λ −1/2 =<br />

„<br />

(1 − θ 0 ) ln` 1 ´ 1 − θ 0 ´«1/2<br />

exp`−θa , so that when θ i → θ 0 there exists an exponentially<br />

θ a(θ i − θ 0 )<br />

θ 0<br />

thin layer in which the transition for Λ −1/2 = constant to Λ −1/2 = ∞ occurs, Ed.

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