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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.12. GENERAL EQUATIONS FOR THE COMBUSTION WAVE 165<br />

On the other hand, consi<strong>de</strong>ring that 8<br />

and<br />

Y j = M j<br />

M m<br />

X j (6.117)<br />

ρ = pM m<br />

RT , (6.118)<br />

the elimination of v di , v dj , Y j and ρ between these three last equations and (6.115),<br />

finally gives the following system of diffusion equations in the form which will be<br />

applied to the solution of the flame equations<br />

dX i<br />

dx = mRT<br />

p<br />

l∑<br />

j=1<br />

(<br />

)<br />

1 ε j ε i<br />

X i − X j , (i = 1, 2, . . . , l). (6.119)<br />

D ij M j M i<br />

Energy equation<br />

The energy equation is the one give in Eq. (3.74), when we disregard in it the terms<br />

due to kinetic energy and viscosity, thus reducing it to the following<br />

m<br />

l∑<br />

j=1<br />

ε j h j − λ dT<br />

dx<br />

where e is a constant <strong>de</strong>fined by the initial or final conditions.<br />

= e, (6.120)<br />

Before transforming this equations into the form in which it will be applied we<br />

shall first consi<strong>de</strong>r the boundary conditions.<br />

Boundary conditions<br />

These conditions are analogous to those applied in the case of two chemical species,<br />

namely,<br />

Cold boundary, x → −∞:<br />

T → T 0 , ε i → ε i0 , X i → X i0 ,<br />

dT<br />

dx → 0, dε i<br />

dx → 0, dX i<br />

→ 0. (6.121)<br />

dx<br />

Hot boundary, x → +∞:<br />

T → T f , ε i → ε if , X i → X if ,<br />

dT<br />

dx → 0, dε i<br />

dx → 0, dX i<br />

→ 0. (6.122)<br />

dx<br />

8 See Chap. 1, Eq.1.34

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