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Untitled - Aerobib - Universidad Politécnica de Madrid

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

to the study of combustion. The extrapolation of the obtained values to the case of a<br />

spray is difficult. In fact, it is necessary to know the size distribution of the droplets<br />

and the composition of the surrounding atmosphere. Furthermore, in or<strong>de</strong>r to account<br />

for the convection effects, which are very important, the motion of the droplets relative<br />

to the atmosphere must also be known. The available information is not sufficient to<br />

show the way in which this extrapolation can be performed [34].<br />

The evaporation velocity of a droplet when convection is absent can be easily<br />

obtained from the formulas <strong>de</strong>duced in the preceding paragraphs. In fact, assuming<br />

that the droplet is isothermal, it is enough to make use of the equations corresponding<br />

to the interior region, enlarged to infinity. Therein the following boundary conditions<br />

must be satisfied which <strong>de</strong>termine the integration constants<br />

r → ∞ : T → T ∞ , Y 1 → Y 1∞ , (13.87)<br />

where Y 1∞ is the mass fraction of the fuel vapours at great distance from the droplet.<br />

Moreover, if one keeps the assumptions previously established with respect to the law<br />

of variation of the values of the transport coefficients as functions of temperature, the<br />

two equations for T and Y 1 are Eqs. (13.53) and (13.54), that is<br />

The last equation when applied to the droplet surface r = r s gives the following<br />

relation<br />

4πr 2 λ ∞<br />

T<br />

T ∞<br />

dT<br />

dr − mc p1T = m(q l − c p1 T s ), (13.88)<br />

4πr 2 (ρD 12 ) ∞<br />

T<br />

T ∞<br />

dY 1<br />

dr = −m(1 − Y 1). (13.89)<br />

The solution of this system that satisfies conditions (13.87) is<br />

1<br />

r = 4πλ (<br />

∞<br />

1 − T + q l − c p1 T s<br />

ln c )<br />

p1(T − T s ) + q l<br />

, (13.90)<br />

mc p1 T ∞ c p1 T ∞ c p1 (T ∞ − T s ) + q l<br />

( ) δ<br />

1 − Y 1 cp1 (T − T s ) + q l<br />

=<br />

. (13.91)<br />

1 − Y 1∞ c p1 (T ∞ − T s ) + q l<br />

(<br />

) δ<br />

1 − Y 1s<br />

q l<br />

=<br />

. (13.92)<br />

1 − Y 1∞ c p1 (T ∞ − T s ) + q l<br />

Let p 1s be the partial pressure of the fuel vapour on the droplet surface. Thermodynamics<br />

shows 13 that p 1s is <strong>de</strong>termined by the temperature T s on the droplet surface.<br />

13 See Prigogine, I. and Defay, R.: Chemical Thermodynamics. Longmans Green & Co., 1954, pp. 332<br />

and f.

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