Nuclear Engineering and Design 121 (1990) 1-10
North-Holland
1
VOID WAVE DISPERSION IN BUBBLY FLOWS *
J-W. P A R K , D.A. D R E W and R.T. L A H E Y Jr.
Department of Nuclear Engineering & Engineering Physics, Rensselaer Polytechnic Institute, Troy, N Y 12180-3590, USA
and
A. C L A U S S E
Centro Atomico Bariloche, 8400 Bariloche, Argentina
Received 1 November 1989
A linear dispersion relationship is derived using a one-dimensional two-fluid model to investigate void wave dispersion in
bubbly flows. This dispersion relationship includes generalized forms of the kinematic wave speed, the characteristics of the
system of equations and the relaxation time. The relaxation time turns out to be a key parameter for the void wave dispersion.
By using appropriate constitutive relations for bubbly flow, the kinematic wave speed and the characteristics are found. The
Froude number is found to be the crucial parameter for void wave dispersion. That is, for two-phase flows with large slip
between the phases (the small Froude number case) the dispersion effect is negligible and thus the kinematic wave
approximation is valid. However, as the relative velocity decreases (the large Froude number case), void wave dispersion
becomes pronounced. In the limit for zero relative velocity, void waves propagate at the same celerity as the characteristics for
homogeneous conditions. The model presented herein also shows the existence of a complementary kinematic wave which is
related to the kinematic wave speed and the characteristics.
1. Introduction
W a v e p r o p a g a t i o n p h e n o m e n a in two-phase flow has been extensively studied since transient response
and even some steady-state behavior (e.g., choking and flooding) are often controlled by the p r o p a g a t i o n
of disturbances. Moreover, the propagation of void fraction disturbances (i.e., void waves) is p r e s u m a b l y
responsible for flow regime transition [1]. In addition, since it has also been f o u n d that the properties of
void waves strongly depend on the constitutive relations (i.e., the closure laws) used in two-fluid models
[2,3], two-phase flow constitutive relations can be developed a n d / o r assessed b y investigating void waves.
The concept of kinematic waves in two-phase flow has been discussed b y Wallis [4], and an extensive
kinematic model for void waves was presented by Bour6 [5].
P a u c h o n and Banerjee [6] have derived an analytical expression for the characteristics of a two-fluid
model which supposedly quantified the d y n a m i c behavior of void waves. Unfortunately, the available
experimental data [2,6,7] have too m u c h scatter to allow one to properly assess such models. However, it is
k n o w n that in two-phase systems the characteristics are basically responsible for p r o p a g a t i n g high
frequency signals which decay faster than the lower frequency signals which are p r o p a g a t e d at the
kinematic wave speed. Nevertheless, except for the studies of Bout6 et al. [8] and Ruggles et al. [3] no
previous investigators have seriously studied frequency dependency on the void wave speed (i.e., the
dispersion of void waves).
In this study, a linear dispersion relationship is derived from a one-dimensional two-fluid model to
investigate the void wave dispersion. This dispersion relationship includes generalized forms of the
* Originally presented at the 26th ASME/AIChE National Heat Transfer Conference, Philadelphia, PA, August 6-9, 1989.
0 0 2 9 - 5 4 9 3 / 9 0 / $ 0 3 . 5 0 © 1990 - Elsevier Science Publishers B.V. ( N o r t h - H o l l a n d )
2
J-V~ Park et al. / Void wave dispersion in bubbly flows
In this study, a linear dispersion relationship is derived from a one-dimensional two-fluid model to
investigate the void wave dispersion. This dispersion relationship includes generalized forms of the
kinematic wave speed, the characteristics and the relaxation time. Using appropriate constitutive relations,
the kinematic wave speed and the characteristics for bubbly flows are found. The influence of some
important parameters, such as Froude number and virtual mass coefficient, on void wave dispersion has
been systematically investigated.
2. T h e o r y
2.1. Basic equations
A one-dimensional two-fluid model for adiabatic and incompressible air/water flow in a constant area
duct can be written using the conservation of mass and momentum equations for both phases:
aak
a
(1)
3-7- + ~ ( a ~ u k ) =0,
[ auk
auk l
Op k
Pk [--gi- + uk-aT-z ] =
az +
A p k i 00~ k
ak
Oz
7"ki Oa k
ak
Oz
1
a
v
Mk,
-
cos o +
ak
4 rk.,
Dn
ak
(2)
where, ML, = --MG, = a c ( F D + Fvm + FR), and, Ap< =Pk, --Pk"
By convention [9] the interfacial momentum transfer term has been partitioned into the interfacial drag
( F D), the virtual mass force (F~m) and a force due to bubble pulsation ( F R). In this study, the force due to
bubble pulsation was neglected since it is normally only important near bubble resonance [9]. Such
phenomena are of interest for pressure waves but not for void waves.
Convenient dimensionless forms of eqs. (1) and (2) are:
oak
at* +
(3)
(akut) =0'
[ ouZ
, o u t l = _ ~apt + apt,
Oak
-a , 0z*
P~[ Ot* + uk a z * J
m
- 9~ cos O + - -
k,•
ak
~*
k, aak
1 a
a z * + a-;
v*
)
%*,,,, 4
(4)
ak Fro,
where,
ut=
M *ki
Uk
URo,
t* ---- g t,
URo
Mk,
~-~'--
PLg '
Z*
---
g
U2Ro Z,
Pt
Pk
PLU2o '
"rk
q.~ = ---'--'~'
PL UR~
Pk
pa~ = -PL
-,
gDH
Fr0=
2 ,
URo
U~=(UG0--UL0 ).
2.2. Linearization
When the two-phase system is disturbed about a fully developed steady-state condition, the perturbed
variables satisfy the following:
J- W. Park et al. / Void wave dispersion in bubbly flows
38%
- 3t*
-
38%
38u'~
* - -OZ*
+
-}- Uko
[ 0Buff
%o
(5)
=0,
OZ*
0Buff ]
3
Apk* o 3 8 %
38p'~
p~[ a - r ' - + u:0 o 7 1 =
3:*
%o
8M;,
M *ko
+--
OZ*
%o
4
3Z*
T*
08r=~
-~- -%o
-OZ
- * -[-
OZ*
"~*wo 1
~- aak/.
&'k*w
%2 8 % -- ~gro
ko
%o
T*o 0 8 %
r~z~
r k,o
* 08ak
%o
%o
(6)
J
To achieve closure, the constitutive relations must be expressed in terms of the state variables, u~, u~ and
a(0/= % = 1 - %). Thus, we assume that the force perturbation on the right hand side of eq. (6) can be
expressed as:
OF* = 0F*30/ o 80/+ ~0F* o 8u~. + 0F*3u~ oOU~.
(7)
Equation (7) can only be used for the algebraic interfacial and wall transfer laws. Other 'forces' such as
those due to virtual mass, must be treated differently. The nondimensional virtual mass force can be
modeled as [10]:
rc,_--~.*_--f°u~
3u~ 3u~
Ou~]
*
"vm=
-vm[ "dt* + U°'dz z"
Ot* - - U *L- - az*
(8)
w
.I
From eq. (8), we obtain the perturbation in the virtual mass force as,
[3aug
38u~
*
afv,~=Cv,..[
at* +u*Go o~*
08u~
or*
u * 38u~/
- -
(9)
Lo az* j"
If we neglect the interfacial pressure difference for the gas phase (Ap~, = 0), we obtain
8 PG* - 8 P t = 8 A P t , ,
(10)
where the surface tension between phases is neglected (i.e.: p~, =PL,). If we subtract the perturbed
momentum equation of the gas phase from that for the liquid phase and eliminate gradients in the velocity,
and the phase average pressure perturbations by using the linearized phasic continuity equations and eq.
(10), we obtain,
380/
380/
328%
3280/
028%
K 1 0 ~ - + K2 0-ff~- + K3 0~--2 + K 4 3 t * 0z* + K s Oz*2 - 0 ,
where,
K1
1(1
(
1-%
1 - % 3u~
1
1_ 3Ow
% 1 % 0u~
K2
1 )411(1
)
% au~ o +ff~0 ~
u*G° 0Fr~ 0.)
a o 3u~
4
1 [ O,~wl
U*Lo O,¢w
+ff~o ~ / ~ ] o
+ 1-a----~ Ou~ o
1 (o~& I
1 -% 0u~
1 3rdw
% 3u~ o
1 [ 0FO[ + u*L° 3Fr~' o
1 - % o / 30/ Io 1---a o 3u~
%[
(lla)
u*Lo O,&o
00/ ]o + 1-%---o 3u[
(11b)
F *Do )2
(1-a o
Uoo*0,tw )
%
u*(3o O~w /
%
% 3u~ o
0u~ o
/
Lwo
~*
0u~ o] + ( 1 - % ) 2
-I- Gw°
(11c)
4
J-W. Park et aL / Void wave dispersion in bubbly flows
K3
- - 1 + - - p~
+
1 - ao
ao
U l__~0
K4=2
Gym
ao(1 _ a o ) 2 '
U*
Cv m [ UI*0
+ p~--~o° + 1 - - a o ~ l _ a o
a0
(lle)
'
,.2
( u#
Lo + . Go + Cvm
1-a------o P6 a o
1-aotl-ao+-~o.
*
T*
T*
~(--ApLi--TzzL +'rzzG)
+
Oa
a0
/
u.:)
.
Go
ApL~o
+
*
zzL
T* + G )
T-
Lio + TZZL0
+
1-a o
--T,* + T*
Gio q'ZZGo
0~0
T*
U*Lo ~(--ApLi--'rZZL +'rzTG)
I0 + 1 - a~o
U*Oo 3 ( _ A p L , * -
* -- T*
0(--ApL,
+ _ _1
1 - ao
Ou~
T*
0u~
u.2
T*
TZZL+TZzG)
]
u*Go
+ ao
%:0)
1 ~ ( __ APL,
. - ~':~L
T* +
K5
(lld)
Ou~
0
O"
(11f)
Ou~
Equation (11a) can be rewritten in more convenient form as:
03a
08a
Ot-----~+ a * -ff~-c + T
.( 0
r. 0__3_i( 0
r.~]
-~-¢ + - Oz . ] ~ -O-~ + + 0 z , ] 6 a = 0 ,
(12)
where,
a+*= a +/URo = K z / K 1,
(13)
T * = K3/Ka,
(14)
r:~= uRo
2K3 -
4- K--;3] -
~
"
(15)
It can be shown [11] that a*+, r2 and T * are the dimensionless forms of the kinematic wave speed,
characteristics and the relaxation time, respectively. It is interesting to note that eq. (12) is similar to, but
more general than, previous results [12].
In summary, the assumptions used to obtain eq. (12) were:
(1) All nonlinear effects are neglected.
(2) Interracial momentum transfer due to bubble pulsation is neglected.
(3) The surface tension between phases and the interracial pressure difference for the gas phase are
neglected.
2.3. Dispersion relationship
The dispersion relationship can be obtained by assuming a solution of eq. (12) in the form:
~Ot = or' e i(~*z*-°'*t*).
(16)
Inserting eq. (16) into eq. (12), we obtain the following linear dispersion relationship:
i(w* - a ' x * ) + T * ( w * - r * x * ) ( w * - r ' K * ) = 0.
(17)
J- IV. Park et aL / Void wave dispersion in bubbly flows
5
Cot
Cox wave
+
a+
F+
..................
*¢
a+
r+
........................................
•
~
a_
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
C~ wave
r*
...........................
C ~x w a v e
/
.............. _~_._......................
a* ~
[
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
0
~R
0
;
"- r-OR
!
a)]i'
;
"
a
t-
Ir
! +
J Co~ w a v e
",r a+
~
I
+
C o~ w a v e
I
r+
+°"
s+'<_,+
T
0
. . . . . .
il!
,
,
O
j
"",,
"t". . . . . . . . . .
-:72
. . . . . . . . . . . . . .
I
!
~
I
!'",,
-1
2¢
I
i
2 T*
C~ w a v e
!
',
i /
C/x w a v e
I
Fig. 1. Plot of eqs. (18) and (19)/(21) for r* < a* < r* (stable).
"',,,,
Ii
'.1
Fig. 2. Plot of eqs. (18) and (19)/(21) for a* > r* (unstable).
If we consider the region where eq. (12) is hyperbolic (i.e., where r~ are real), the solution of eq. (17) for
traveling waves (i.e., where k* is real) can be found by solving the following coupled equations.
1 [a:-,
~-~"
~0~' = 2 T *
]
1 ,
~0~2_ C*= [
( a * - ?)2 - (C* - ?) 2
- 4 T ' 2 ( C * ---r )_-: 2-77:~
(C~. .r *.) (.C.* - r * )
(18)
]
,
(19)
where,
~* = ~a~ + ivan,
(20)
c * = ,o~/K*,
(21)
~= (r* + r* )/2.
(22)
One finds from eq. (19) that void wave dispersion is pronounced for large values of the relaxation time
(T * ), since the wave speed ( C * ) is strongly dependent on angular frequency when relaxation time is large.
It is interesting to plot eqs. (18) and (19). As shown in figs. 1 and 2, two speeds of propagation are
possible (i.e., C+ and C~- waves) for a specified frequency. The larger one (C+) is easily recognized as the
6
J-W. Park et al. / Void wave dispersion in bubblyflows
predominant speed of propagation since it is close to the kinematic wave speed (a+*). However, a
complementary void wave (C~-) is also present. The dispersion relationship implies that the Ca wave is
slower and has relatively high damping, as shown in figs. 1 and 2. The complementary kinematic wave
speed, the counterpart of the classical kinematic wave speed, (i.e., C~- at zero frequency) can be found
from eq. (19) as:
lira
C * = a _* --
r +*
+ r _*
(23)
a+*
.
-
tOR~0
The well-known stability criteria [11] for C~+ waves can be easily found by examining the solid lines in
figs. 1 and 2 as:
(24)
r*<a+
3.
Solutions
and
discussion
Appropriate constitutive relations must be used to quantify the properties of void waves. The drag
force, FD, for bubbly flow can be modeled as:
L
FD = PL~--~n(UG -- UC)lug -- uL l,
(25a)
where the interfacial friction factor for undistorted bubbles is given by [13]:
D H 1 + 0.1 Re°~75
Rez,
f, = 18 Db
(25b)
with,
Re2
=
L(l --
PL(UG +
UL)Db
+
,
D b : bubble diameter.
(25c)
The interfacial pressure difference for the gas phase has been neglected (ApG ' = 0), while for the liquid
phase,
ApE ` = --'r/Pc(U G -- UL)2.
(26)
The value ~/= ~ can be derived using potential flow theory. It is good assumption that the interfacial shear
and the Reynolds stress for the gas phase is negligible (~-Gi= ~rTo= 0). However, for the liquid phase, we
assume that the interfacial shear is equal to the bubble-induced Reynolds stress:
% , = ZTzzL = - - k a O L
( UG --
UL) 2"
(27)
Biesheuvel et al. [14] have found that, k = ½.
Since the gas phase is dispersed in the liquid phase, the wall shear due to the gas phase is negligible
(rG,~ = 0). The wall shear due to the liquid phase is,
.rL,~ = f w p L
(28)
u2.
Using these constitutive relations and eqs. (13) and (15), we can obtain the dimensionless forms of the
kinematic wave speed and the characteristics in a frame referenced to the liquid phase velocity:
A~_
a + - UL0 -= 1-URo
nao,
(29a)
J- W. Park et aL / Void wave dispersion in bubbly flows
7
where,
+aO)r~_woDb/4.5ODn]Re2, o
[ao'r~woDb/2.25DHU~o] Re2, o
4.5 +0.3375 Re°752,o+ [(1
1 + 0.1750 Re2°,7o5+
(29b)
and
r_+-- ULo
G - -u~
= V* + v~f~-/~'*,
(30a)
where,
V * zx (1 - or0) [ g y m - ~J - ko~ 0 + p~(1 - a0)]
=
%(1 - % ) + Cvm
(30b)
'
r * & %(1 - % ) + Cvm + pa(1 - %)2,
P* ~ ( 1 - - O~0) 2
(30c)
.
2
[Cvm - ~J - ko¢ 0 + P G ( 1 -- Or0) ]
. . . . . . . . .
+
[%(1 -%)
+ 2(1 - 0/0)2(7/-
-'~---~"~-2
Cvm+ 06(1- %) ]
Cvm/2)
-- 1 0 ; ( 1
+ao(1-ao)(n+k-Cvm)
(30d)
-- o¢0) 3.
It should be noted that eqs. (30) reduce to the results of Pauchon and Banerjee [12] if we let: fw = 0,
p ~ = 0 , C~m= ½, r/=-~ and k = ~ .
If we neglect the wall shear stress in eq. (29b), we find that 1.93 _< n _< 4.5 for all values of Re2, o. To
bound the possibilities, the dimensionless kinematic wave speeds given by eq. (29a) for n = 1.93 and
n = 4.5 are shown in fig. 3 with the characteristics. According to the stability criteria given by eq. (24), the
kinematic wave is stable over a wide range of Re2%. More specifically, since Re2¢o0 is proportional to
relative velocity, n is increased as the relative velocity is decreased. Thus, the kinematic wave can be
stabilized by reducing the phasic slip in the steady flow. It should be noted that since Re2, ° is also
proportional to the size of bubbles, small bubbles stabilize the kinematic wave.
The dimensionless relaxation time can be found by eq. (17):
T*- gV_ FroRe2,o
[ao(1-ao)+Cvm+P~(1-ao) 2]
Up,o 18DH/Db 11 + 0.175 Re °7'2q~o+(aOrtwoDb/2.25DHU¢o)Re2~0]
(31)
"
As can be seen in eq. (31), the Froude number (gDH/U2o) strongly influences the void wave relaxation
time. As shown in fig. 4, the void wave is nondispersive for Fr o = 2.7 (UR0 = 30 c m / s ) which means that
void wave propagation in a stagnant pool of liquid can be well described by the kinematic wave
approximation. However, as can be noted in eq. (18), as the Froude number increases void wave dispersion
becomes pronounced and damping (or amplification) decreases. It should also be noted that since
relaxation time is not very sensitive to void fraction, the mean void fraction does not strongly influence
void wave dispersion.
As mentioned earlier, the dispersion relationship presented herein has a complementary kinematic wave
(a_). Using the constitutive relations previously discussed and eq. (23), we find that the dimensionless
speed of the complementary kinematic wave is:
A*_
a - ULo
- -)t*+X*_-A*.
URo
(32)
J- W. Park et al. / Void wave dispersion in bubbly flows
8
/ . A_ (n=4.5)
/
1.0
/
A+, A+
0.5
50
x+
7-
o
r
0
:::
O0
A* (n=1.95)
T
i
b!
LJ
27
]
I
f
\
-0.5
I
/./
I
\\ A*+ (n=4.5)
05
Fig. 4. D i m e n s i o n l e s s relaxation time (Cvm = 0.5,
D H = 2.54 cm, D b = 1 cm).
Fig. 3. Characteristics and kinematic w a v e speeds (Cvm = 0.5,
T/= 0.25, k = 0.2, r~w° = 0, ~ = 0).
0.5
0
i
i
k
i
of
i
i~
o C rqq/'Is
CrN J~
co I
(I/~)
J
j"
I0 c m / s
-10
Fig, 5. T e m p o r a l d a m p i n g of the a _ w a v e (Cvm = 0.5, T~w° = 0, Dr~ = 2.54 cm, D b = 1 cm).
h*wo=0,
J- W. Park et al. / Void wave dispersion in bubbly flows
9
As shown in fig. 3, the coalescence of kinematic wave speeds (i.e., A*+ - A * ) occurs at a lower void
fraction than where the characteristics coalesce (i.e., X* = ?,*) if the corresponding a+ wave is stable.
If we use eqs. (18) and (32), we can obtain the damping of the a_ wave as
(.01 : 18
urn[1 +0.175 Re°75 +
(ao'r~woDb/2.25Dn)Re2,o]
2~°
Db[a0(1 -- % ) + Cvm + 0~(1 -- Or0) 2] Re24, o
(33)
The damping of the a_ wave given by eq. (33) is plotted in fig. 5 for different UR0. AS can be seen, the a
wave has large temporal damping when the phasic slip is large. Thus, based upon the constitutive relations
used herein, it appears to be possible to observe the a_ wave when phasic slip is small.
The unique features of the a wave (i.e., the complementary kinematic wave) - can be summarized as:
(1) Its speed is determined by both the kinematic wave speed and the characteristics.
(2) It is always stable independent of the stability of kinematic waves (i.e., a + waves).
(3) It may have large temporal damping.
4. Summary and conclusions
It has been shown that the linear dispersion model appears to be able to quantify void wave dispersion.
According to our model, void wave dispersion is pronounced for large values of the relaxation time, which
is determined by Froude number, the virtual mass coefficient and the void fraction. Since the relaxation
time is small for large values of the relative velocity (i.e., where the Froude number is small), void waves in
a stagnant pool of liquid can be successfully described by a kinematic wave model. However, since
relaxation time increases as relative velocity decreases (i.e., the Froude number becomes large), the void
waves become more dispersive when slip is reduced. The virtual mass effect also promotes void wave
dispersion since the relaxation time is increased as the virtual volume coefficient is increased.
The stability of the kinematic wave was analyzed based on our model. The kinematic was shown to be
stable when the slip a n d / o r the bubble-size are reduced.
The dispersion model presented herein yields a complementary kinematic wave speed which is
determined by the kinematic wave speed and the characteristics. The complementary kinematic wave (i.e.,
the a_ wave) propagates in the flow direction in a frame of reference fixed to the liquid phase with
damping if the corresponding kinematic wave is stable. It should be noted that, to date, no experimental
verification of the presence of the complementary void wave ( a _ ) has been made. However, since the
coalescence of the eigenvalues (i.e., ~ * = ~,*) signals the threshold for ill-posedness, and eq. (32) implies
the following relationship at that point,
A*= 2?t*-A~.
We see that the onset of ill-posedness may be measurable if A* can be measured. Thus, it appears that
further research on the complementary void wave may yield important insights into such phenomena as
flow regime transition. It is hoped that this paper will help stimulate such research.
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Grenoble (1987).
10
J-I'lL. Park et al. / Void wave dispersion in bubbly flows
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