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Untitled - Aerobib - Universidad Politécnica de Madrid

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168 CHAPTER 6. LAMINAR FLAMES<br />

and<br />

q j =<br />

h j<br />

c p T f<br />

. (6.134)<br />

In comparison with the case of only two chemical species, we observe here the appearing<br />

of a set of parameters Λ ij . However, all these parameters have only one unknown<br />

quantity, the value of m, this is to say the flame velocity, therefore the set Λ ij may be<br />

expressed as a function of just one of the parameters.<br />

Diffusion equations<br />

l∑<br />

( )<br />

Mi<br />

L ij X i ε j − X j ε i<br />

dX<br />

M<br />

i<br />

dθ = j=1<br />

j<br />

, (i = 1, 2, . . . , l), (6.135)<br />

l∑<br />

θ − 1 + q j (ε j − ε jf )<br />

j=1<br />

where<br />

L ij =<br />

λRT<br />

M i c p pD ij<br />

, (6.136)<br />

Boundary conditions<br />

The boundary conditions reduce to the following<br />

θ → θ 0 : ε i → ε i0 , X i → X i0 , (6.137)<br />

θ → 1 : ε i → ε if , X i → X if . (6.138)<br />

Like in the case of two chemical species the difficulty at the cold boundary may be<br />

eliminated by introducing an ignition temperature θ i whose value does not influence<br />

the result when the reduced activation energies θ aj , or at least some of them, are large<br />

as normally happens in practical cases for the same reasons stated in <strong>de</strong>tail in the two<br />

species case.<br />

A recount of the number of boundary conditions when compared to the number<br />

of equations proves that the conditions are superabundant and hence, an eigenvalue of<br />

m, this is, one of the values of Λ ij , must exist which makes compatible the said<br />

conditions and therefore the problem is essentially the same than in the case of two<br />

species only.

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