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Untitled - Aerobib - Universidad Politécnica de Madrid

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13.16. APPENDIX: APPLICATION OF PROBERT’S METHOD 331<br />

13.16 Appendix: Application of Probert’s method for<br />

the combustion of fuel sprays<br />

Probert 15 has <strong>de</strong>veloped a theoretical method for the study of evaporation or combustion<br />

of fuel sprays, un<strong>de</strong>r the assumption that evaporation constant is the same for all<br />

droplets. The justification of this assumption and the value that should assigned to the<br />

constant if it is valid, <strong>de</strong>pend on the results the experimental measurements.<br />

After chapter 13 was written, some theoretical works on the application of<br />

Probert’s method have been performed at the I.N.T.A. 16 corresponding to steady burning<br />

as well as to transition from ignition to steady burning and periodic combustion.<br />

In these computations the size distribution function of Mugele-Evans was used with<br />

preference to those of Rosin-Rammler and Nukiyama-Tanasawa, since it allows the<br />

prediction of the sizes with a very good approximation taking into account the maximum<br />

size of the droplets. Let F be the mass fraction of fuel corresponding to droplets<br />

with a diameter smaller than d. Mugele-Evans’ formula gives for F the following<br />

expression<br />

F = 1 2<br />

( (<br />

))<br />

θd<br />

1 + erf ε ln<br />

. (13.108)<br />

d max − d<br />

Here erf is the error integral, d max is the droplet’s maximum diameter and ε and θ<br />

are two parameters characteristic of the distribution. Fig. 13.9 shows some of the<br />

distributions corresponding to typical values for these parameters. It is seen that the<br />

increment of ε increases the uniformity of the spray, whilst when θ increases the mean<br />

diameter of the droplets reduces.<br />

Let G be the volume of fuel, injected to the burner per unit time, and g the<br />

volume of the droplets existing in the burner. It can be verified that g is expressed as a<br />

function of G through formula<br />

where I is given by expression<br />

I =<br />

∫ 1<br />

0<br />

x 4 dx<br />

∫ 1 − x<br />

0<br />

g = εI √ π<br />

G t v , (13.109)<br />

−<br />

e<br />

(<br />

p ) 2<br />

x2 + y<br />

ε ln<br />

1 − p x 2 + y<br />

and t v is the life time of the largest droplets of the spray.<br />

(x 2 + y)<br />

(1 5/2 − √ ) dy, (13.110)<br />

x 2 + y<br />

15 Probert. R.P.: The Influence of Spray Particle Size and Distribution in the Combustion of Oil Droplets.<br />

Philosophical Magazine, February 1946.<br />

16 Millán, G., and Sanz, S.: Analysis of the Combustion Processes in Gas Turbines. Fourth International<br />

Congress of Combustion Engines, Zurich, 1957.

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