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Untitled - Aerobib - Universidad Politécnica de Madrid

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276 CHAPTER 11. SIMILARITY IN COMBUSTION. APPLICATIONS<br />

Maximum blowoff<br />

velocity (ft/s) φ m<br />

2.0<br />

1.5<br />

1.0<br />

600<br />

400<br />

200<br />

100<br />

10<br />

2 4 6 8 10 2 4 6 8 10<br />

Reynolds number<br />

3 4 5<br />

Figure 11.3: Maximum blowoff velocity and corresponding equivalence ratio for a cylindrical<br />

flame hol<strong>de</strong>r.<br />

Maximum blowoff velocity (ft/s)<br />

1000<br />

800<br />

600<br />

400<br />

300<br />

200<br />

150<br />

100<br />

4<br />

2.5 4 6 8 10 1.5 2 3 4 6 8 10 5 1.5<br />

Reynolds number<br />

Figure 11.4: Maximum blowoff velocity for different types of flame hol<strong>de</strong>rs (see [22] for<br />

more <strong>de</strong>tails).<br />

Both figures show clearly the existence of a transition Reynolds number, approximately<br />

equal to 10 4 , which separates two different regions. For Re < 10 4 , the<br />

maximum blowing velocity corresponds to a composition different from the stoichiometric<br />

one, which furthermore varies with the Reynolds number, whilst if Re exceeds<br />

the transition number the composition remains constant. Likewise, for Re > 10 4<br />

the blowing velocity varies with the square root of the Reynolds number, while for<br />

Re < 10 4 it follows a different law.<br />

Zukoski and Marble, Ref. [17], have <strong>de</strong>monstrated that such a change is due to<br />

the fact that the free boundary layer of the mixing zone changes from laminar to turbulent.<br />

This transition is important because the transfer of heat and chemical species between<br />

unburnt gases and combustion products, within the mixing zone, occurs through<br />

laminar diffusion un<strong>de</strong>r subcritical conditions and through turbulence in the opposite<br />

case.

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