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Untitled - Aerobib - Universidad Politécnica de Madrid

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6.10. STRUCTURE OF THE COMBUSTION WAVE 159<br />

in which case the only un<strong>de</strong>termined parameter would be a 1 to be obtained when<br />

comparing the value for ( dε/ dθ) θ=1 given by (6.98),<br />

( ) dε<br />

= θ a − a 1 , (6.105)<br />

dθ<br />

θ=1<br />

with the one resulting from (6.67)<br />

( ) dε<br />

(1 − θ 0 = ( )<br />

dθ<br />

θ=1<br />

dε<br />

(1 − θ 0 )<br />

dθ<br />

θ=1<br />

The following second-<strong>de</strong>gree equation will be obtained for a 1<br />

. (6.106)<br />

− 1<br />

1 − θ 0<br />

θ a − a 1 = Λ<br />

(1 − θ 0 )(θ a − a 1 ) − 1 , (6.107)<br />

which when solved gives the value of the un<strong>de</strong>termined parameter, which in turn,<br />

when taken into (6.100) provi<strong>de</strong>s the <strong>de</strong>sired approximation for J.<br />

Therefore, this approximation of J <strong>de</strong>pends on Λ, and when introduced into<br />

(6.73.a), it supplies an equation for Λ, whose solution gives the eigenvalue which<br />

solves the problem.<br />

6.10 Structure of the combustion wave<br />

Once <strong>de</strong>termined the value of Λ which makes compatible the boundary conditions of<br />

the flame equations, a simple numerical integration of such equations, through any of<br />

the methods available, will give the distribution of temperature, concentrations, etc.<br />

through the combustion wave. If the integration is performed by using system (6.67),<br />

(6.68), the curves obtained will be as those shown in Fig. 6.9. When the structure is<br />

<strong>de</strong>sired on a physical plane it is sufficient to integrate the system of equations (6.64),<br />

(6.65) and (6.66). However for this case one must select the position of origin of coordinates<br />

which is un<strong>de</strong>termined. Fig. 6.13 shows the solution corresponding to the case<br />

represented in Fig. 6.9. It is seen that the structure is analogous to the one represented<br />

in Fig. 6.4, corresponding to the simplified case discussed in §6. Fig. 6.13, shows a<br />

dot-line representation of the distribution of temperatures corresponding to the case of<br />

pure thermal conduction, where chemical reaction is absent, which practically coinci<strong>de</strong>s<br />

with the wave up to a θ = 0.5, proving that up this point the action of chemical<br />

reaction is extremely small.<br />

the same<br />

As a characteristic length of the phenomenon it was adopted, for its solution,<br />

l = λ f<br />

mc p<br />

(6.108)

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