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.

138 CHAPTER 6. LAMINAR FLAMES<br />

The equations for the heating and diffusion zone, x < 0, may be obtained<br />

from those given §2 by introducing in them the conditions expressing the absence of<br />

chemical reaction, that is: w = ε = 0. There resulting<br />

Heating and diffusion zone, x < 0.<br />

ρD dY<br />

dx<br />

The corresponding boundary conditions are<br />

= mY, (6.15)<br />

λ dT<br />

dx = mc p(T − T 0 ). (6.16)<br />

x = −∞ : T → T 0 , Y → 0, (6.17)<br />

x = 0 : T = T i . (6.18)<br />

Since for x → −∞ both dY / dx and dT / dx tend to zero, as it can be verified<br />

by taking (6.17) into (6.15) and (6.16), the introduction of an ignition temperature<br />

eliminates the difficulty at the cold boundary. Furthermore by comparing the equations<br />

for the heating and diffusion zone with those for the reaction zone, given in the<br />

preceding paragraph, and the boundary conditions (6.13) and (6.18), it may be readily<br />

verified that the transition from one zone to another at point x = 0 is continuous for<br />

all variables when adopting the additional condition that the value for Y at x = 0,<br />

which is un<strong>de</strong>termined, be the same for both solutions<br />

x = 0 : Y (0 − ) = Y (0 + ). (6.19)<br />

The objection to this way of <strong>de</strong>aling with the difficulty at the cold boundary<br />

states that the solution obtained, and in special the propagation velocity for the flame,<br />

will <strong>de</strong>pend on the value adopted for T i , which does not actually exist. Nevertheless, it<br />

will be proved further on, when studying the solutions for the combustion wave, that as<br />

long as the velocity of the chemical reaction <strong>de</strong>pends substantially on the temperature<br />

of the mixture, it will happen that the solution obtained will be in<strong>de</strong>pen<strong>de</strong>nt from the<br />

values of T i , except for values of this temperature very close to T 0 or to T f . Un<strong>de</strong>r<br />

such conditions the influence of the ignition temperature will vanish completely from<br />

the result, when calculating the propagation velocity of the flame.<br />

The presence of a flame hol<strong>de</strong>r<br />

Another solution proposed to the problem of the cold boundary consists in imagining<br />

the presence of a flame hol<strong>de</strong>r placed in front of the wave which has the double mission

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

Saved successfully!

Ooh no, something went wrong!