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Next: Wall shear stress
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Void fraction
In this section we derive the void fraction model originally introduced by Zuber
and Findlay. We will consequently call the model the Zuber-Findlay void fraction
model. This model is chosen on the following grounds
- The model has found a wide acceptance in the nuclear industry.
- The model includes effects of non-uniform cross-sectional void
distribution.
We introduce the local drift velocities, ugj and
[
], by the following expressions
 |
(6.49) |
and
 |
(6.50) |
These velocities express the phase velocities relatively to the center of volume
velocity j (the total volumetric flux, (6.3)).
The local drift fluxes, jgj and
[
], are
defined by
 |
(6.51) |
 |
(6.52) |
and express the volumetric fluxes of vapor and liquid, respectively, through a
cross-sectional plane moving with the velocity equal to the center of volume
velocity j.
Now, using these newly introduced quantities we can derive the Zuber-Findlay void
fraction model. Using the identity
 |
(6.53) |
and averaging over the cross-sectional area (see (6.7)) we obtain
 |
(6.54) |
The fundamental assumption is that the local quantities
and j may
vary across the cross section such that, in general,
 |
(6.55) |
Since we are not interested in the local variation we define the
correlation coefficient
 |
(6.56) |
which is called the distribution parameter6.8 [--] and a new
velocity
 |
(6.57) |
which is called the drift velocity [
].
Physically the distribution parameter accounts for the non-uniform distribution
of void and flow whereas the drift velocity accounts for the local slip between
the two phases and is closely related to the terminal rise velocity of the vapor
phase through a stagnant liquid.
Introducing the correlation coefficients (6.66) and
(6.67) in the averaged equation (6.64) yields
 |
(6.58) |
or
 |
(6.59) |
For practical calculations it is useful to express
in terms
of the averaged flow quality
.
According to the last expression
in (6.21) we have
 |
(6.60) |
and
 |
(6.61) |
Inserting these quantities into (6.69) we obtain
![\begin{displaymath}
\mbox{$<\!{\alpha}\!>$} = \frac{ \frac{1}{\rho_g}
\mbox{$<...
...\mbox{$<\!{x}\!>$}}{\rho_\ell} \right]
+ \overline{u}{}_{gj}}
\end{displaymath}](img1215.gif) |
(6.62) |
and dividing by
we obtain the Zuber-Findlay void fraction
model
![\begin{displaymath}
\mbox{$<\!{\alpha}\!>$} = \frac{\mbox{$<\!{x}\!>$}}{ C_0\le...
...t] + \frac{ \rho_g
\overline{u}{}_{gj}}{\mbox{$<\!{G}\!>$}} }
\end{displaymath}](img1217.gif) |
(6.63) |
Upon comparing (6.73) with the general void fraction expression
(6.24) we note that the slip implicitly given in the Zuber-Findlay
void fraction model,
,
is
 |
(6.64) |
In order to use the Zuber-Findlay void fraction model we have to specify the
quantities C0 and
through external constitutive relations.
We find a myriad of different correlations for C0 and
in the
literature.
One of the proven set of correlations for normal BWR-operation, ie
co-current upwards flow, consists of
the one by Dix [18, p. 207] for C0 which states
![\begin{displaymath}
C_0 = \mbox{$<\!{\beta}\!>$}\left( 1 + \left[ \frac{1}{\mbox{$<\!{\beta}\!>$}} - 1
\right]^b \right)
\end{displaymath}](img1222.gif) |
(6.65) |
where the exponent b is defined by
![\begin{displaymath}
b \;\hbox{$=$\kern-0.68em\raise1.1ex
\hbox{$\scriptscriptstyle\triangle$}}\;\left[ \frac{\rho_g}{\rho_\ell} \right]
\end{displaymath}](img1223.gif) |
(6.66) |
and
is defined by
 |
(6.67) |
The correlation for
given by Lahey and Moody [18]
states
![\begin{displaymath}
\overline{u}{}_{gj} = 2.9 \left[ \frac{ (\rho_\ell-\rho_g)\sigma
g}{\rho_\ell^2}\right]^{1/4}
\end{displaymath}](img1227.gif) |
(6.68) |
External constitutive relations exist which are applicable to every flow, ie for
low-flow or counter-current flow as well as normal BWR-operation
conditions [30]. However, in general use of these relations require
iterative solutions and consequently are more impractical to use [31, p. 6-1].
Next: Wall shear stress
Up: External
Previous: External
  Contents
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