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Untitled - Aerobib - Universidad Politécnica de Madrid

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13.8. DIFFUSION EQUATIONS 313<br />

13.8 Diffusion equations<br />

To compute the distribution of the mass fractions of fuel vapours and oxygen, the<br />

equations (13.14) and (13.25) must be integrated. For this v 1 and v 3 must be expressed<br />

as functions of the mixture velocity v and of the mass fractions Y 1 and Y 3 by using the<br />

diffusion equations. Both the interior and exterior region will be studied separately.<br />

Interior region r s ≤ r ≤ r l<br />

The continuity equation 13.14) for the fuel vapour can be written in the form<br />

4πr 2 ρY 1 (v + v d1 ) = m, (13.40)<br />

where v d1 is the diffusion velocity of the fuel vapours through the atmosphere of inert<br />

gases. Fick’s law, 5 gives for this velocity<br />

v d1 = − 1 Y 1<br />

D 12<br />

dY 1<br />

dr , (13.41)<br />

where D 12 is the diffusion coefficient for the fuel vapours and the inert gases.<br />

When Eq. (13.41) is substituted into Eq. (13.40) and Eq. (13.10) is taken into<br />

account, one obtains<br />

4πr 2 ρD 12<br />

dY 1<br />

dr = −m(1 − Y 2) (13.42)<br />

for the <strong>de</strong>termination of Y 1 . The integration constant for this equation is <strong>de</strong>termined<br />

by expressing that the mass fraction of the fuel vapours at the flame is zero<br />

r = r l : Y 1 = 0, (13.43)<br />

Exterior region r ≥ r l<br />

This procedure applied to Eq. (13.25) gives the following equation for the distribution<br />

of oxygen in the exterior region of the flame<br />

4πr 2 ρD 23<br />

dY 3<br />

dr = m(ν + Y 3). (13.44)<br />

The solution to this equation must satisfy the condition that on the flame front mass<br />

fraction of oxygen must be zero,<br />

r = r l : Y 3 = 0, (13.45)<br />

which <strong>de</strong>termines the value for the corresponding integration constant.<br />

5 See chapter 2.

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