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Untitled - Aerobib - Universidad Politécnica de Madrid

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290 CHAPTER 12. DIFFUSION FLAME<br />

Moreover, as done in the theory of free jets, here only some terms of the viscosity<br />

forces need to be preserved. 4<br />

2) The influence of mass forces is important. Hydrostatic equilibrium in the fluid<br />

undisturbed by the flame <strong>de</strong>termines the pressure field. If ρ 0 is the <strong>de</strong>nsity of the<br />

undisturbed fluid<br />

−∇p + ρ 0 ¯F = ¯0, (12.5)<br />

which gives for Eq. (12.3)<br />

ρ(¯v · ∇)¯v = ∇ · τ ev + (ρ − ρ 0 ) ¯F . (12.6)<br />

Furthermore, in each case only the significant terms of ∇ · τ ev will be retained. So<br />

far a solution that inclu<strong>de</strong>s the influence of the last term of Eq. (12.6) has not been<br />

obtained.<br />

Energy equation<br />

Kinetic energy of motion, energy dissipated by viscosity and work done by mass<br />

forces are negligible. Hence, equation (3.38) reduces to<br />

(<br />

ρ(¯v · ∇)h − ∇ · (λ∇T ) + ∇ · ρ ∑ )<br />

Y i h i¯v di = 0. (12.7)<br />

i<br />

Diffusion equations<br />

Such equations are given by system (3.8) which takes the form<br />

∑<br />

(<br />

Y j ¯vdi − ¯v dj<br />

+ ∇Y i<br />

− ∇Y )<br />

j<br />

= ¯0, (i = 1, 2, . . . , l)<br />

M<br />

j j D ij Y i Y j<br />

∑<br />

Y j ¯v dj = ¯0,<br />

j<br />

(12.8)<br />

where pressure and thermal diffusion are not inclu<strong>de</strong>d since they are negligible.<br />

State equation<br />

This is equation (3.39)<br />

p<br />

ρ = R mT. (12.9)<br />

4 See Fay, Ref. [15].

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