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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.9. SOLUTION OF THE FLAME EQUATIONS 151<br />

will be written for shortness as<br />

∫ 1<br />

( ) n<br />

λ 1 − Y<br />

I =(1 − θ 0 ) θ δ−n e −θ 1 − θ<br />

a<br />

θ dθ, (6.74)<br />

λ f 1 + aY<br />

J =<br />

∫ 1<br />

0<br />

θ i<br />

(1 − θ) dε. (6.75)<br />

With this notation, the fundamental Eq. (6.73) may be written<br />

1 − θ 0<br />

2<br />

− J = ΛI.<br />

The following is a separate study of both approximations.<br />

(6.73.a)<br />

Approximation of integral I<br />

Heat transfer λ is a function of temperature θ of the mixture and its composition<br />

<strong>de</strong>fined by the value of Y . 6 Consequently, in or<strong>de</strong>r to calculate I the problem reduces<br />

to finding an approximation for Y as a function of θ. The solution <strong>de</strong>pends on the<br />

value of the Lewis-Semenov number.<br />

Lewis-Semenov number equal to unity<br />

If L = 1, then Y is a lineal function of θ in the following form<br />

In fact, when condition<br />

Y = θ − θ 0<br />

1 − θ 0<br />

. (6.76)<br />

L ≡<br />

is satisfied, the diffusion Eq. (6.65) may be written in the form<br />

λ<br />

ρDc p<br />

= 1 (6.77)<br />

λ dY<br />

dx = mc p(Y − ε). (6.78)<br />

By adding to it the energy Eq. (6.66), multiplied by an arbitrary constant C,<br />

λ d<br />

(<br />

dx (Y + Cθ) = mc p Y + C(θ − θ 0 ) − ( C(1 − θ 0 ) + 1 ) )<br />

ε . (6.79)<br />

This equation is satisfied i<strong>de</strong>ntically with the following two conditions<br />

6 See Chap. 2, §4.<br />

C(1 − θ 0 ) + 1 = 0, (6.80)<br />

Y + C(θ − θ 0 ) = 0, (6.81)

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