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Untitled - Aerobib - Universidad Politécnica de Madrid

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13.11. NUMERICAL APPLICATION 319<br />

where r si is the initial radius. This formula is the fundamental result of the present<br />

theory.<br />

The combustion time t c of a droplet of radius r si is, obviously,<br />

t c = r2 si<br />

k . (13.75)<br />

The position r l /r s of the flame front is obtained by writing T = T l in Eq. (13.62).<br />

Furthermore if m/r s is eliminated from the result by means of Eq. (13.73), one obtains<br />

r l<br />

r s<br />

=<br />

1 − T l<br />

T ∞<br />

+<br />

kρ e c p<br />

2λ ∞<br />

q ln q − c . (13.76)<br />

pT ∞<br />

c p T ∞ q − c p T l<br />

Therefore, the radius of the flame and the droplet are proportional.<br />

Formula (13.73) enables the study of the influence of the physical constants of<br />

the fuel and the state of the surrounding atmosphere on the burning rate of the droplet. 8<br />

In particular, the said formula shows that the heat transmitted from the flame to the<br />

droplet surface is the <strong>de</strong>termining factor for its burning velocity. This is due to the<br />

fact that the burning rate of the droplet is <strong>de</strong>termined by the heat received by the same.<br />

Therefore, the essential factor in the combustion process is not the volatility of the fuel<br />

but its heat of evaporation. Experiments results confirm this conclusion. In fuels at the<br />

high temperature reached when combustion occurs, the evaporation mechanism differ<br />

essentially from the evaporation when the temperature of the surrounding atmosphere<br />

is normal. In the last case the evaporation is maintained by the diffusion of the vapors<br />

from the droplet towards the exterior. The evaporation velocity is <strong>de</strong>termined by the<br />

difference between the vapour pressures on the droplet surface and at infinity. 9<br />

13.11 Numerical application<br />

The above formulas are applied here to the study of the combustion of a gasoline<br />

droplet in the air. The following typical values are adopted<br />

T ∞ = 300 K, T s = 355 K, ρ c = 0.85 gr/cm 3 ,<br />

λ ∞ = λ s = 55 × 10 −6 cal/cm s K, q l = 95 cal/gr, q = 10 000 cal/gr,<br />

c p1 = 0.60 cal/gr K, c p2 = 0.35 cal/gr K, c p3 = 0.26 cal/gr K,<br />

Y 3∞ = 0.23, ν = 3, δ 1 = δ 2 = 0.9.<br />

8 Information on the subject can be found in Godsave’s works [19].<br />

9 See §15, Eq. (13.103).

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