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Untitled - Aerobib - Universidad Politécnica de Madrid

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12.1. INTRODUCTION 283<br />

In fact, otherwise, some of the species would diffuse across the flame and react with<br />

those on the other si<strong>de</strong>.<br />

In or<strong>de</strong>r to judge the validity of this mo<strong>de</strong>l Hottel and Hawthorne [3] performed<br />

some experiments to <strong>de</strong>termine the composition of the gases in a diffusion flame of<br />

hydrogen burning in the open atmosphere, taking samples of the gas at different points<br />

of the flame by means of a special sound. Details of these experiments can be found<br />

in the said work. Figure 12.2, taken from it, shows the results of the sounding ma<strong>de</strong><br />

in three cross sections of the flame. The results of such measurements prove the<br />

correctness of Burke and Schumann’s mo<strong>de</strong>l.<br />

100<br />

75<br />

50<br />

25<br />

H 2<br />

flame front<br />

distance from port= 30.5 cm<br />

Percentage in dry sample<br />

0<br />

100<br />

75<br />

50<br />

25<br />

0<br />

100<br />

O 2<br />

H 2<br />

N 2<br />

N 2<br />

axis of flame<br />

flame front<br />

O 2<br />

distance from port= 22.85 cm<br />

75<br />

50<br />

25<br />

H 2<br />

N 2<br />

flame front<br />

distance from port= 15.25 cm<br />

0<br />

O 2<br />

0 10 20 30 40<br />

Radial distance (mm)<br />

Figure 12.2: Gas composition in a hydrogen diffusion flame<br />

Burke and Schumann have successfully applied their mo<strong>de</strong>l to the calculation<br />

of the shape and height of laminar diffusion flames for the case where the fuel jet<br />

discharges within a tube where an air stream moves with the same velocity than the<br />

fuel jet, Fig. 12.3. This <strong>de</strong>vice eliminates the difficulties originating from momentum<br />

transfer between the fuel and the surrounding air when their velocities are not equal.<br />

Furthermore, for this reason it is easier to obtain a stable flame. By introducing several<br />

drastic simplifications, to be consi<strong>de</strong>red further on, Burke and Schumann were able<br />

to calculate the shape of the flame. Some of their results are outlined in Fig. 12.3.<br />

Fig. 12.3 (a) corresponds to an overventilated flame, which closes at the axis of the

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