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Untitled - Aerobib - Universidad Politécnica de Madrid

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154 CHAPTER 6. LAMINAR FLAMES<br />

whose solution is<br />

θ ≃ 1 : 1 − Y ≃ L<br />

1 − θ 0<br />

(1 − θ), (6.86)<br />

this approximation must replace Eq. (6.76) when L is different from unity and furthermore<br />

the value taken for L must be that corresponding to the temperature and<br />

composition of the hot boundary conditions of the flame, T = T f .<br />

If the activation energy has a small value and an approximation of Y vs θ that<br />

will be valid within a wi<strong>de</strong>r range of temperatures is <strong>de</strong>sired, then the linear approximation<br />

(6.86) may be substituted by the following parabolic<br />

Y ≃<br />

( θ − θ0<br />

1 − θ 0<br />

) L<br />

, (6.87)<br />

which for θ = 1 coinci<strong>de</strong>s with (6.86) and for θ ≃ θ 0 it behaves like the solution<br />

corresponding to the heating zone (ε ≡ 0). This can readily be verified. Fig. (6.10)<br />

shows some of the curves (6.86) and (6.87).<br />

1.0<br />

0.8<br />

L=0.5<br />

L=0.75<br />

0.6<br />

L=1.5<br />

L=2.0<br />

Y<br />

0.4<br />

L=1.0<br />

0.2<br />

0.0<br />

0.125 0.2 0.4 0.6 0.8 1.0<br />

θ<br />

Figure 6.10: Linear and parabolic approximations of Y vs θ given by Eqs. 6.86 and 6.87<br />

for θ 0 = 0.125.<br />

The preceding consi<strong>de</strong>rations prove that it is generally sufficient, when calculating<br />

the integral to take for λ/λ f the value unity which corresponds to the hot<br />

boundary, or some other approximation at the neighborhood of this point. Frequently<br />

the following approximations are used<br />

λ<br />

λ f<br />

≃ θ,<br />

λ<br />

λ f<br />

≃ √ θ. (6.88)

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