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Untitled - Aerobib - Universidad Politécnica de Madrid

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332 CHAPTER 13. COMBUSTION OF LIQUID FUELS<br />

1.0<br />

F<br />

0.9<br />

0.8<br />

0.7<br />

0.6<br />

0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

(0.5,1.5)<br />

(1.5,1.0)<br />

(1.0,1.0)<br />

(1.5,1.5)<br />

(1.0,1.5)<br />

(1.0,0.5)<br />

(0.5,0.5)<br />

(0.5,1.0)<br />

(1.5,0.5)<br />

0.0<br />

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0<br />

d / d max<br />

Figure 13.9: Droplet size distribution without combustion according to Mugele and Evans<br />

(fraction F of droplets with a diameter smaller than d/d max), for several values<br />

of the parameters (ε , θ).<br />

Magnitu<strong>de</strong> (13.109) is interesting since the combustion intensity of the burner<br />

should be consi<strong>de</strong>red inversely proportional to it.<br />

Table 13.2 gives the values for g/G t v for three typical cases corresponding to<br />

θ = 1.<br />

ε 0.5 1 1.5<br />

g<br />

0.129 0.110 0.105<br />

G t v<br />

( )<br />

ds<br />

0.269 0.438 0.895<br />

d max<br />

spray<br />

(<br />

ds<br />

d max<br />

)flame<br />

0.517 0.454 0.401<br />

Table 13.2: Values of g/Gt v for θ = 1 and ε = 0.5, 1, 1.5.<br />

It is seen that when ε increases, that is when the uniformity of the spray increases,<br />

the mass fraction of fuel in the burner <strong>de</strong>creases. Consequently, it is advantageous<br />

to work with spray as uniform as possible in or<strong>de</strong>r to <strong>de</strong>crease the volume of<br />

the primary zone of the burner.

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