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Untitled - Aerobib - Universidad Politécnica de Madrid

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208 CHAPTER 7. TURBULENT FLAMES<br />

(a) Time exposure photograph<br />

(b) Instantaneous Schlieren photograph<br />

Figure 7.1: Stoichiometric natural gas-air flame, Re = 25 000, burner tube diameter =<br />

5.08 cm (by courtesy of Bureau of Mines).<br />

preference was given to the use of the mean surface between those internally and externally<br />

limiting the luminous zone [3] or else to the surface where luminosity reaches<br />

its maximum intensity [4].<br />

Additional difficulty lies in the fact that the paths of the gas particles are not<br />

known. Therefore it is risky to i<strong>de</strong>ntify the fraction of unburnt mixture corresponding<br />

to each element of the flame front. Such difficulty has often been elu<strong>de</strong>d by measuring<br />

the mean velocity obtained when the total flow rate of the mixture is divi<strong>de</strong>d by the<br />

area of the flame front. The propagation velocity of turbulent flames has been measured<br />

with these or similar techniques by Damköhler [2] , Bollinger and Williams [3],<br />

Scurlock [4], Williams, Hottel and Scurlock [5], Karlovitz, Denniston and Wells [6],<br />

Wohl, Shore, von Rosemberg and Weil [7], Leason [8], Bowditch [9], Wohl and Shore<br />

[10], Mickelsein and Ernstein [11], etc.<br />

Figure 7.2 taken from Ref. [3] shows, as an example, the results of the measurements<br />

performed by Bollinger and Williams in mixtures of several hydrocarbons<br />

and air. For each case the mixture giving the maximum velocity was used. This figure<br />

also shows the laminar velocities corresponding to the same mixtures. It is seen that<br />

the effect is maximum in the acetylene flame where the value of the laminar flame ve-

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