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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.4. MODIFICATION OF THE CONDITIONS AT THE “COLD BOUNDARY” 137<br />

6.4 Modification of the conditions at the “cold<br />

boundary”<br />

There are several solutions available in or<strong>de</strong>r to elu<strong>de</strong> the difficulty of the cold boundary,<br />

which has passed unnoticed until recently. The history of the evolution of thought<br />

on this subject may be followed by consulting references [17] through [19]. Herein<br />

we will only study the two solutions currently used, which consist in introducing an<br />

ignition temperature T i and a flame hol<strong>de</strong>r.<br />

Ignition temperature<br />

By adopting the same assumption used in the classical theories of Combustion, that<br />

is, by assuming that there is an ignition temperature T i , such that reaction velocity of<br />

the mixture is zero for T < T i , this temperature divi<strong>de</strong>s the combustion wave into<br />

two zones: a “heating and diffusion zone”, corresponding to temperatures un<strong>de</strong>r T i , at<br />

which no chemical reaction takes place, and a “reaction zone”, which corresponds to<br />

temperatures over T i .<br />

The differential equations for the reaction zone are the same given in the preceding<br />

paragraph, which are summarized in the following, as well as the boundary<br />

conditions, assuming that the origin of coordinates x = 0 is located at ignition point<br />

T = T i .<br />

Reaction zone, x > 0.<br />

m dε = w(Y, ρ, T ), (6.2)<br />

dx<br />

ρD dY<br />

dx<br />

= m(Y − ε), (6.3)<br />

λ dT<br />

dx = mc p<br />

The boundary conditions for this system will be<br />

(<br />

(T − Tf ) + (T f − T 0 )(1 − ε) ) . (6.5.a)<br />

x = 0 : ε = 0, T = T i , (6.13)<br />

x → +∞ : ε = 1, T = T f , Y = 1. (6.14)

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