21.11.2014 Views

Untitled - Aerobib - Universidad Politécnica de Madrid

Untitled - Aerobib - Universidad Politécnica de Madrid

Untitled - Aerobib - Universidad Politécnica de Madrid

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

148 CHAPTER 6. LAMINAR FLAMES<br />

Once Λ is known then the velocity u 0 of the flame is given by<br />

√<br />

Bλ f e<br />

u 0 =<br />

−θa<br />

ρ 2 0 c p(1 − θ 0 ) Λ−1/2 . (6.72)<br />

6.9 Solution of the flame equations<br />

As before said, the preceding system cannot by integrated analytically. Hence, it<br />

becomes necessary to resort either to numerical solutions or else to semi-analytical<br />

approximation methods.<br />

The numerical methods are very cumbersome since we are <strong>de</strong>aling with an<br />

eigenvalue problem with given boundary conditions at both extremes of the interval,<br />

and, therefore, we would have to make numerous tentatives before reaching the exact<br />

solution. Generally, the use of electronic computers is required and in particular they<br />

were wi<strong>de</strong>ly utilized by Hirschfel<strong>de</strong>r and his collaborators.<br />

In recent years, several approximate methods have been proposed generally<br />

based in the unusual behavior of the solutions due to the presence of factor e −θa/θ in<br />

the reaction velocity. In fact, when the reduced activation temperature θ a is large, as<br />

should be expected in combustion reactions, due to this factor the result is <strong>de</strong>termined,<br />

essentially, by the form of the solution close to the hot boundary and this enables<br />

the <strong>de</strong>velopment of methods, as those proposed by Zeldovich-Frank-Kamenetskii-<br />

Semenov [4] and the one by Boys-Corner [5], Adams [20], Wil<strong>de</strong> [21] and von Kármán<br />

[6], with different variations and approximations. Only very recently a comparative<br />

study of these methods has been performed. Information on the subject will be found<br />

in the work by von Kármán [10] and, specially, in the more complete study carried<br />

out by Millán, Sendagorta and Da Riva [22]. Figures 6.5 and 6.6, taken from this<br />

study show a comparison between the approximate values for Λ −1/2 ( to which the<br />

flame velocity is proportional by virtue of (6.72)), obtained through several of those<br />

methods, with the exact value, given by a numerical integration. This comparison was<br />

performed for several values of the temperature of the unburnt gases and of the activation<br />

energy of the reaction. All the results shown in these figures correspond to a<br />

Lewis-Semenov number equal to unity and to a constant mean molar mass of the mixture.<br />

However, the unpublished results of the calculations performed for more general<br />

cases indicate that the same conclusions are still valid.<br />

Figures 6.5 and 6.6 show that the Boys-Corner method in its first iteration<br />

gives <strong>de</strong>fect values with an important <strong>de</strong>viation. The same happens with the method<br />

by Zeldovich et al., but giving excess values. The approximation improves with the

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!