Accepted Manuscript
Mechanistic modeling of critical sand deposition velocity in gas-liquid stratified flow
Ramin Dabirian, Ram S. Mohan, Ovadia Shoham
PII:
S0920-4105(16)31228-1
DOI:
10.1016/j.petrol.2017.06.006
Reference:
PETROL 4018
To appear in:
Journal of Petroleum Science and Engineering
Received Date: 5 December 2016
Revised Date:
13 April 2017
Accepted Date: 2 June 2017
Please cite this article as: Dabirian, R., Mohan, R.S., Shoham, O., Mechanistic modeling of critical sand
deposition velocity in gas-liquid stratified flow, Journal of Petroleum Science and Engineering (2017),
doi: 10.1016/j.petrol.2017.06.006.
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Mechanistic Modeling of Critical Sand Deposition Velocity
in
Gas-Liquid Stratified Flow
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Ramin Dabirian
Tulsa University Separation Technology Projects
McDougall School of Petroleum Engineering
The University of Tulsa
Tulsa, OK, USA
ramin-dabirian@utulsa.edu
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Ram S. Mohan
Tulsa University Separation Technology Projects
Mechanical Engineering Department
The University of Tulsa
Tulsa, OK, USA
ram-mohan@utulsa.edu
Abstract
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Ovadia Shoham
Tulsa University Separation Technology Projects
McDougall School of Petroleum Engineering
The University of Tulsa
Tulsa, OK, USA
ovadia-shoham@utulsa.edu
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Among the different regimes in multiphase pipelines, stratified flow is most prone to sand
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deposition, owing to the low liquid velocity and the lack of mixing. The main goal of this study
is to predict the critical sand deposition velocity under stratified flow. The critical sand
deposition velocity is defined as the minimum velocity that keeps all particles moving at all time,
above which there is no stationary bed at all.
Two models with similar approaches are developed based on the forces acting on a
particle, such as the drag, turbulent, apparent gravity, van der Waals and lift forces for prediction
of the transitions between moving/stationary dunes and moving/stationary bed. Dune pilling up
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and collapsing mechanism considering a torque balance on a rolling particle located at the top of
the dune is adopted for stationary dunes. Torque balance applied to a rolling particle located on
the lowest stratum of the moving bed layer is used to predict the minimum liquid film velocity
Comparison between the predictions of the two
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for particle to grow a stationary bed.
mechanistic models and the experimental data show good agreement, with critical sand
deposition velocity absolute relative errors at 16.4% for stationary dunes and 12.6% for
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stationary bed.
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Introduction
Solid particle hydraulic transport is one of the methods that has been applied by the
industry for many years for handling sand generated during petroleum production. This mode of
operation is environmentally friendly and also has low operation and maintenance costs.
Research on sand transport in multiphase flow has recently gained attention in the Petroleum
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Industry, as it has some important applications. These include cutting transport in wellbore,
abrasive slurry jet drilling (Padsalgikar, 2015), and sand transport in multiphase flow pipeline
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(Dabirian et al. 2016). Several researchers attempted to extend the modeling of liquid-solid flow
to gas-liquid-solid flow. However, in multiphase flow, owing to the complexity of the physical
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phenomena, various flow patterns occur, such as stratified, slug, annular and dispersed bubble.
As the each of the flow patterns exhibits a different sand transport mechanism, extension of
models developed for liquid-solid flow to gas-liquid-solid flow is questionable.
Liquid-Solid Flow: Durand and Condolios (1952) developed the first correlation for the
minimum liquid velocity needed to suspend particles in horizontal pipeline. A series of equations
to predict the critical velocity for slurry flow was developed by Thomas (1962), considering the
ratio the particle diameter to viscous sub-layer thickness. Later, a model based on the forces
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acting on a single particle was developed by Wicks (1971), suggesting that the moment created
by lift, drag, and buoyancy forces that cause a single particle to rotate should overcome moment
created by gravity force. Oroskar and Turian (1980) developed a correlation for critical velocity
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to keep a particle suspended, based on isotropic turbulence theory, considering the component of
the energy in the vertical direction versus gravity. A model for minimum velocity to keep
particles completely suspended in the liquid phase was developed by Davies (1987). He stated
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that only eddies with approximate size of particles are effective in particle transport.
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A two-layer model for prediction of the “limit of stationary deposition velocity” (critical
velocity) was developed by Wilson et al. (1992). The model is based on an equilibrium between
driving and resisting forces, which act on a sand bed. It is widely applied for hydraulic transport
of solid in pipeline, especially for the sliding bed regime. Similarly, Doron et al. (1987)
developed a 2-layer model for the prediction of limit of stationary deposition velocity. Later,
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Doron and Barnea (1993) extended the Doron et al. (1987) model to a 3-layer model, including
both a stationary bed layer and a moving bed layer on top of it. The 3-layer model resolved the
poor prediction of the critical velocity, obtained by the 2-layer model, for low slurry flow rate.
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Lahiri (2010) developed a model to predict the critical suspension velocity based on 800
The model was developed utilizing artificial neural
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data points collected from literatures.
network and support vector regression. More recently, Miedema (2012) published a
comprehensive book on slurry transport fundamentals and historical overview. Also presented is
an outstanding framework for slurry transport, which is applicable for dredging operation using
water as the carrier liquid and sand or gravel as the solids. The framework includes a
methodology to determine the slurry head loss, as well as the limit deposit velocity, for spatial
volumetric concentration.
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Gas-Liquid-Solids Flow: Holte et al. (1987) modified the Wicks (1971) model developed
for liquid-solid flow, extending it to stratified flow. A similar approach was presented by Salama
(2000), for the critical sand deposition velocity to completely suspend particles in the liquid
0.04
⋅d
0.17
P
⋅υ
−0.09
L
∆ρ
⋅
ρL
0.55
⋅ D0.47 .......................................................................................... (1)
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VM ,C
V
= SL
VM
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phase, by applying the liquid superficial and mixture velocities, as follows
where VM,C is the critical mixture velocity needed to suspend all particles. Note that the effect of
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particle concentration is not considered in this model.
Another extension of single phase liquid model for the critical velocity to gas-liquid flow,
utilizing the drift flux model, was presented by Danielson (2007). The author assumed constant
(terminal) velocity between the solid particles and the liquid phase, ignoring the effect of particle
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concentration. The developed correlation for the critical velocity, VC , for particle suspension is
as follows
−1 / 9
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VC = 0.23υ L ⋅ d P1/ 9 ⋅ ( g ⋅ D ⋅ (s − 1)) 5 / 9 ............................................................................................ (2)
where s is the density ratio of solid to liquid phases.
A model for the prediction of the minimum velocity needed to completely suspend the
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particles, based on force balances on a particle in vertical and horizontal directions, was
published by Ponagandla (2008). The drag and lift force coefficients were solved iteratively,
utilizing the Stokes’ equation and the turbulent velocity fluctuations. Hill (2011) developed a
correlation to predict the minimum velocity required to keep all particles moving, extending the
Oroskar and Turian (1980), which utilizes the liquid film velocity instead of the single phase full
pipe velocity, namely
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= 1.85CV
g d P ( ρ P / ρ L − 1)
where
N Re =
0.1536
Dρ L g d P ( ρ P / ρ L − 1)
µL
(1 − CV )
0.3564
dP
D
−0.378
N Re
0.09
................................................. (3)
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VC
..................................................................................................... (4)
where CV is the particle volume concentration.
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Ibarra et al. (2014 and 2016) developed an empirical correlation to predict the minimum
mixture velocity for sand deposition in stratified flow, combining both Oroskar and Turian
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(1980) and Salama (2000) models. The correlation includes four empirical constants obtained by
regression analysis of the acquired experimental data and a modification of Chisholm (1976)
liquid holdup, yielding
−0.378
VSL
−35.49 d P
0.09
= 1.3277⋅
⋅ (1 − CV )
⋅
⋅ N Re,
........................................... (5)
crit
g d P ( ρ P / ρ L − 1)
D
VM ,crit
where NRe,crit is given in Equation (4).
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VM ,C
As can be seen from the literature review, previously published models were developed
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for “bed” in general, not distinguishing between Stationary Dune and Stationary Bed. Based on
the current study data (refer to Figure 1) these two configurations have different particle
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deposition mechanisms. The current study analyzes these two configurations separately,
developing the deposition velocities for these two sand flow regimes.
The critical sand
deposition velocity is defined as the minimum velocity that keeps all particles moving at all time,
above which either the dune or bed is sliding, whereby below it either one is stationary.
The previously published studies for gas-liquid-solid are either empirical correlations,
extensions of liquid-solid models or semi-mechanistic models. On the other hand, the current
study includes two mechanistic models, based on the physical phenomena, for Stationary Dunes
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and Stationary Bed separately. In general, mechanistic models can be scaled up with more
confidence, as compared to either empirical or semi-mechanistic models. The developed models
include the important flow variables, some of which were neglected by previous studies, such as
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liquid viscosity, particle size and concentration, stratified flow characteristics (liquid holdup and
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phase velocities).
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Figure 1. Stratified Flow Sand Regimes for Stationary Particles
Modeling
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In this study, two models are developed for prediction of the critical sand deposition
velocity, including the transitions between Moving Dunes - Stationary Dunes and Moving Bed -
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Stationary Bed. Both proposed models are based on a torque balance derived from the forces
acting on a particle. For the transitions between Moving Dunes - Stationary Dunes the analyzed
particle is located on top of the dune, while for the transition between Moving Bed - Stationary
Bed the particle is located at the bottom of the moving bed layer. Dabirian (2016) may be
referred for more details.
Figure 2 presents the flow chart of the approach applied for the prediction of the critical
sand deposition velocities. The proposed models are based on five steps: (1) For a given
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superficial liquid velocity, the superficial gas velocity is reduced step by step. Correspondingly,
the liquid holdup ( H L ) is predicted by using the Taitel and Dukler model (1976) with stratified
wavy interfacial shear stress with an interfacial friction factor of f I = 0 .0142 ; (2) The liquid
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film velocity, which is the critical sand deposition velocity, is calculated by VL =VSL / HL ; (3) The
forces acting on the particle, including the drag, turbulent, apparent weight, van der Waals and
lift forces are determined; and (4) Equating the net torque balance to zero, the resulting liquid
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velocity is identified as the critical sand deposition velocity.
Figure 2. Computational Algorithm for Critical Sand Deposition Velocity
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Liquid Holdup
Taitel and Dukler (1976) model is the most applicable model used for characterizing
stratified wavy flow in industry. The model is developed from a combination of gas and liquid
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momentums, and the combined momentum is an implicit equation for the liquid level in the pipe.
The model is applicable for steady-state, fully-developed, and Newtonian flow, and the
wettability effect is ignored. Gas-liquid interface is assumed to be flat, and the liquid holdup is
τ WG
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momentum of gas and liquid phases calculated as
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calculated based on the liquid thickness. The liquid height is calculated based on the combined
1
SG
S
1
− (ρ L − ρ G )g sin (α ) = 0 .......... .......... .......... .......... ..... (6)
− τ WL L + τ I S I
+
AG
AL
AL AG
where S G , S L and S I are the perimeter lengths of the gas, liquid and interface, respectively.
Also, AG and AL represent the cross-sectional area occupied by the gas and liquid phases,
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respectively. ρ G and ρ L symbolize the gas and liquid densities, respectively. τ WG , τ WL and τ I are
gas, liquid and interfacial shear stresses, respectively, and they are determined as
1
f G ρ GVG2 ................................................................................................................... (7)
2
1
τ WL = f L ρ LVL2 ...................................................................................................................... (8)
2
1
τ I = f I ρ G (VG − VI )2 .......................................................................................................... (9)
2
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τ WG =
where V L is the liquid velocity, VG is the gas velocity, and V I is the interface velocity, which is
ignored since VI << VG . f G , f L and f I represent the friction factors for gas, liquid and
interface, respectively. The friction factors for gas and liquid phases are calculated based on
Blasius equations. Taitel and Dukler (1976) suggested that the interfacial shear stress for
stratified smooth is the same as the gas wall shear stress. For stratified wavy flow with small
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amplitude waves, a constant value for f I = 0 . 0142 originally suggested by Cohen and Hanratty
(1968) and later used by Shoham and Taitel (1984) is applied for all cases.
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Forces Acting on Particle
The forces acting on a single particle can be divided into two groups. The first group
includes the forces, such as drag, lift and turbulent, which promote the movement of the particles
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along the pipe. The second group consists of the forces that resist the movement of the particles.
These forces are considered for modeling of the critical sand deposition velocities for both
•
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Stationary Dunes and Stationary Bed. The equations of these forces are presented next.
Drag Force ( FD )
This force is exerted on a particle by the fluid in the same direction of the flow and is
given as
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1
2
FD = ρ L CD APP VLL ......................................................................................................... (10)
2
where ρ L is the liquid density, VLL is the local liquid velocity, APP is the area of the particle
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that is projected on a plane normal to the flow direction and CD is the drag coefficient. The drag
coefficient is determined by White (1991), namely,
24
6
+
+ 0.4 ................................................................................................
ReP 1 + Re2P
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CD =
(11)
The particle Reynolds number, ReP , is defined as
ρ LVLL d P
.................................................................................................................. (12)
µL
where dP is the particle diameter and µL is the liquid dynamic viscosity. It is assumed that the
ReP =
movement of the particle is affected by the velocity profile upstream of it. The local velocity,
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VLL , is calculated based on the “law of the wall” developed by Leif (1972), which is valid
through the viscous sublayer and the turbulent boundary layers. It is defined as
+
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1
1
1
+
+
+
+
+
+
y + = VLL + a ekVLL −1 − kVLL − (kVLL ) 2 − (kVLL )3 − (kVLL )4 .................................. (13)
2
6
24
+
where a = 0.1108 and k is 0.4. The dimensionless distance, y , and V LL , the dimensionless
local flow velocity, are, respectively
............................................................................................................................... (14)
υL
VLL =
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+
y Vτ
VLL
Vτ
............................................................................................................................. (15)
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y+ =
υ L is kinematic viscosity and the friction velocity, Vτ , is calculated by
Vτ = VLL
f
8
.........................................................................................................................
(16)
The moody friction factor, f , is calculated based on Hall (1957) as follows
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1
106 3
4 ε
f = 0.00551 + 2 ×10
+
.................................................................................... (17)
D
Re
For the calculation of the drag force from Eq. 10, the determination of the local velocity,
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VLL , follows Ramadan et al. (2001), as shown schematically in Figure 3.
Figure 3. Velocity Field ahead of Particle
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As shown in the figure, the distance y is taken from the center of the analyzed particle, as
the particle is partially situated between the particles beside it. In Eq. 10, APP is particle
projected area to the flow direction of the upper part of the particle, which is determined by
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πd 2
β sin(2β )
APP = P 0.5 +
+
...................................................................................... (18)
180
2π
4
where β is the repose angle of the particles. Finally, it is proposed that the roughness (ε) used
Turbulent Force ( FT )
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in the calculation of the friction factor in Eq. 17 is approximated by the radius of the particle.
Portion of the turbulence generated by the fluid suspends the particles against gravity.
According to Oroskar and Turian (1980), the turbulence is negligible when either laminar flow
exists in the pipe or the particle size is less than the viscous sublayer ( δ ) . Otherwise, the
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turbulent force is calculated based on the fraction of the turbulent energy that is available to
suspend a particle in the liquid phase. According to this model, it is assumed that part of the
turbulent energy is dissipated as heat, which will not contribute to suspending the particles. Thus,
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the turbulence portion that causes particle suspension is reduced by a factor, w. The turbulent
force and the factor, w, are given by
and
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if Re < 2100 or d P < δ
0,
FT = 1
2
otherwise
4 ρ LVτ AP w,
...................................................................................
4γ 2 ∞
4γ 2
2 2
+ ∫ exp −
dγ ................................................................
γ exp −
π π
π γ
π
The flow Reynolds number is defined as
w=
(19)
(20)
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Re =
ρ LVL d L
µL
.................................................................................................................. (21)
where d L is the liquid phase hydraulic diameter and γ is given by
VS (1 − CV ) 2
υL
.................................................................................................................. (22)
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γ=
C V is the sand concentration and VS is settling velocity, which is calculated as
gd P2 ( ρ P − ρ L )
.............................................................................................................. (23)
18µ L
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VS =
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Apparent Weight Force (FG )
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where ρP is the particle density.
The apparent weight force is the difference between the weight and buoyancy forces,
which is given as follows
•
π d P3
6
g(ρP − ρL ) .......................................................................................................................... (24)
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FG =
Van der Waals Force (FVDW )
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This is attraction force between particles is significant for small particle sizes. According
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to Cabrejos (1991) the van der Waals is defined by
A d
FVDW = H P2 ............................................................................................................... (25)
12 S
where AH and S are, respectively, the Hamaker. Constant and the separation length between
the particle and the wall, which are given by Rabinovich and Kalman (2009), as follows
AH = 6.50×10−20 ................................................................................................................ (26)
S = 6.20 ×10−9 .................................................................................................................... (27)
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Lift Force (FL )
The fraction of pressure and shear stress acting on the surface of the particle constitutes
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the lift force. According to Saffman (1965), small particles experience lift force when the particle
is moving through a relatively high viscous fluid in a low shear flow, as given by
µ V d P2 dVLL
FL = 1.615 L LL
υ L 0.5 dy
........................................................................................... (28)
dVLL
is the local velocity gradient, which is calculated based on Ramadan et al. (2001), as
dy
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where
0.5
dVLL Vτ2 dVLL
=
dy υ L dy +
where
dV LL
dy +
+
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follows
................................................................................................................ (29)
+
is given by Leif (1972) as
+
dVLL
=
dy+
1
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............................................... (30)
1 3 + 2 1 4 +3
kVLL+
+
2
1 + a ke
− k − k VLL − k VLL − k VLL
2
6
where a = 0.1108 and k is 0.4. Wang et al. (1997) modified Saffman’s equation based
on the experimental results collected by Hall (1988), namely,
0.5
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µLVLLd P2 dVLL
F (r + ) .......................................................................................... (31)
FL = 1.615
0.5
υL
dy
+
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+
where F (r ) , as given below, is valid for 1.8 < r + < 100
F (r ) =
20.9 (r + ) 2.31
101.962 log r
+
+ 1.412
.................................................................................................... (32)
and r + is given as
dP υL
+
r =
2 dV LL
dy
−0.5
.......... .......... .......... .......... .......... .......... .......... .......... .......... .......... ........
(33)
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Prediction of Critical Sand Deposition Velocity for Stationary Dunes
Several mechanisms have been proposed for sand transport in pipelines, including
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suspension, sliding (dragging), lifting and rolling. According to Ramadan et al. (2001), the main
mechanisms of transporting particles in flowing fluid are either lifting or rolling. Stevenson et al.
(2002) developed correlations for incipient particle motion velocity for sliding and rolling.
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Ibrahim et al. (2003) considered incipient particle motion velocity for the mechanisms of
suspension, sliding and rolling. Three models for dragging, lifting and rolling were developed by
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Byron et al. (2016), based on force balances for initiating particle motion. According to this
study, two mechanisms, namely, saltation (bouncing) and rolling (climbing) play important roles
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in sand transport, as shown schematically in Figure 4.
Figure 4. Schematic of Rolling and Saltation Mechanisms
Force balances along the flow direction and normal to the flow direction are considered
corresponding to the sliding and lifting forces, which are given, respectively, by
FSliding = FD − FG sin(θ + α ) − F f
............................................................................................ (34)
FLifting = FL + FT − FG cos(θ + α ) − FVWD
.......... .......... .......... .......... .......... .......... .......... ....
(35 )
where (θ ) is the front angle of the dune and (α ) is the pipe inclination angle. Substituting the
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different forces, as defined previously in Eq. (34) and Eq. (35) results in
π d3
1
A d p
2
FSliding = CD ρL APPVLL − FG sin(θ + α) − f K { P g(ρP − ρL ) cos(θ + α) + H 2
2
6
12 S
µL VLL d p2 dVLL
1
F(r + )} .............................................................. (36)
− ρL (Vτ ) 2 AP w − 1.615
0.5
4
υL
dy
FLifting = 1.615
µ L VLL d p2 dVLL
υ L 0.5
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0.5
0.5
π d3
1
F (r + ) + ρ L (Vτ ) 2 AP w − P g ( ρ P − ρ L ) cos(θ + α )
4
6
dy
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A d p
− H 2 ............................................................................................................... (37)
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where f K is the kinematic friction coefficient accounting for the effect of wet lubrication friction
between two particles.
The saltation mechanism is caused by the resultant of the lifting and sliding forces. The saltation
happens only when the resultant angle of FLifting and FSliding is greater than the summation of
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the front angle of a dune (θ ) and pipe inclination angle (α ) , as given by
> (θ + α ) ............................................................ (38)
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FD − FG sin(θ + α ) − F f
arctan
FL + FT − FG cos(θ + α ) − FVWD
Based on the acquired experimental data, Eq. 38 is not valid for dunes, and as a result, saltation
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does not occur in the transition between Moving Dunes - Stationary Dunes.
According to the study of US Geological Survey (Colver, 1998), sand dunes creep on the
pipe bottom based on pilling up and collapsing mechanisms, which are derived by particle
rolling. Figure 5 shows a schematic of the pilling up and collapsing mechanism. As shown in the
figure, the sand particles role and pile up on top of the dune until the front of a dune is so steep
that it collapses under its own weight. The repeating cycle of sand moving up and collapsing
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causes the sand dunes to move forward in the direction of the flow. Collapsing of a dune occurs
when the front angle of dunes (θ ) exceeds a specific value. Based on the study of Colver
(1998), this angle for wet sand is θ = 45º. In this study, it is assumed that the repose angle of
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particle is β = 60°, assuming that the particles are closely packed with nearly equal diameters.
Figure 5. Schematic of Pilling up and Collapsing Mechanism of Sand Dunes
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The directions of the forces depend on the repose angle ( β ) , dune front angle ( θ ) and
pipe inclination angle ( α ) . Figure 6 shows the directions of the forces acting on a particle located
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on the dune.
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Figure 6. Forces Acting on Single Particle for the Case of Sand Dunes
The net torque can represent the rolling tendency of a particle located on the top of a sand
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dune. The torque balance around point O (see Figure 6) is given by
Tnet = L D ( FD ) − LG ( FG ) + LT , L ,VWD ( FT + FL − FVWD ) .......... .......... .......... .......... .......... ....
(39 )
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For the dune case, the following equations represent the levers of the drag force (LD ) ,
turbulent force ( LT ) , lift force (LL ) , Van Der Waals force (LVWD) and apparent weight force (LG) ,
LD =
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namely,
dP
sin (β ) ..................................................................................................................... (40)
2
LT = LL = LVWD = LT ,L,VDW =
LG =
dP
cos(β ) ................................................................................ (41)
2
dP
cos(α + θ − β ) ......................................................................................................... (42)
2
Substituting for the forces and their corresponding levers results in the final form of the net
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torque, as follows
πd 3
dP
d
1
2
sin( β ) C D ρ L APPVLL − P cos (α + θ − β ) P g ( ρ P − ρ L ) .................... (43)
2
2
2
6
1
µ L VLL d p2
dP
2
+
cos( β )
ρ (V ) AP w + 1.615
4 L τ
2
υ L 0.5
dVLL
dy
0.5
A
F (r + ) − H
12
d p
2
S
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Tnet =
To find the transition from Moving Dunes to Stationary Dunes, two conditions must be satisfied:
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1) The net torque balance is zero, which means that no particle rolling happens. In such
conditions, the rolling up torque is equal to the torque that tends to rotate the particle
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downwards.
2) The sand dune is stable, which means the angle of front dune ( θ ) needs to be 0 ≤ 45°,
otherwise, the dune collapses under its weight.
Thus, incorporating the two conditions presented above, Eq. 43 is solved implicitly for VL
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, which represents the critical sand deposition velocity. The effect of concentration on the critical
velocity is considered only in the turbulent force. Since the experiments were conducted at low
concentrations less than 0.00404 m3/m3, the effect of concentration on the turbulent force is not
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significant and can be neglected. Therefore, referring to Figure 4, for this study, the pilling up
and collapsing mechanism is not a function of the particle concentration and the size of sand
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dune; however, it is strongly depends on the steepness of the dune front.
Prediction of Critical Sand Deposition Velocity for Stationary Bed
The modeling approach for the prediction of the critical sand deposition velocity for
Stationary Bed is similar to the one developed for the Stationary Dunes case, which was derived
base on the particle rolling mechanism. However, for the case of Stationary Dunes the analyzed
particle is located on top of the dune. On the other hand, for the Stationary Bed case, the
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analyzed particle is located at the bottom of the lowest stratum of the moving bed layer, and on a
stationary mono-layer of particles, as shown schematically in Figure 7. Thus, for the Stationary
Bed case, the weight of the other particles in the moving bed that are located on the top of the
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analyzed particle is added in the analysis. This gives the value of the maximum liquid velocity,
which causes the first sand particles to stop moving and deposit as a stationary mono-layer of
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particles at the bottom of the pipe.
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Figure 7. Forces Acting on Analyzed Particle for the Case of Sand Bed
The weight force on the particle placed at the lowest stratum of the moving bed layer
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includes the weight of the particle itself and other particles in the moving bed layer on top of it.
Therefore, the average number of solid particles that exists in the moving bed should be
considered. Following Doron and Barnea (1993),
y MB − d P
y
+ 1 = CMB MB + (1 − CMB ) ...................................................................... (44)
dP
dP
and the total submerged weight is found as
N = CMB
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π d P3
y
FG = N FG = C MB MB + (1 − C MB )
g ( ρ P − ρ L ) ........................................................ ( 45)
dP
6
where C MB is the maximum packing of particles (CMB = 0.74) , and y MB is the height of the
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moving bed layer. It is assumed that the moving bed height ( yMB) is proportional to the particle
concentration (CV ) . The acquired experimental results show a correlation between the
yMB
) , and the particle concentration (CV ) , namely,
dP
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dimensionless height of a moving bed, (
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y MB
0.5
= 337.8 (CV − 0.001) ............................................................................................... (46)
dP
The force levers of the lift, drag, turbulent and van der Waals are calculated as before
(Eqs. 40 and 41), while the force lever for the apparent weigh is
LG =
dP
cos(α − β ) ...................................................................................................................... (47)
2
Also, the torque balance for the Stationary Bed case is similar to the torque balance
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calculated for Stationary Dunes (Eq. 43). The following equation is the final form of the torque
balance for the Stationary Bed case:
π d3
dP
y
1
2 d
sin(β ) CD ρ L APPVLL − P cos(α − β ) P g (ρ P − ρ L ) CMB MB + (1 − CMB )
2
dp
2
2
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Tnet =
AC
C
0.5
1
µ L VLL d p2 dVLL
dP
AH d p
2
+
+ cos(β ) ρ L (Vτ ) AP w + 1.615
F
(
r
)
−
2 ....................... (48)
0.5
dy
4
2
12
υ
S
L
Similarly, the net torque balance is set to zero and the equation is solved for V L , which presents
the critical sand deposition velocity for Stationary Bed.
Comparison Study
Two computer codes are developed utilizing MATLAB, based on the models presented
in the previous section. The input for these models/codes include the superficial gas velocity,
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superficial liquid velocity, pipe diameter, pipe inclination angle, liquid viscosity, and particle
size and concentration. The output provides the critical sand deposition velocities for both the
Stationary Dunes and Stationary Bed cases, and their corresponding liquid hold up are
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calculated.
The developed models are compared with the experimental data collected by Dabirian et
al. (2016), as well as the correlation by Ibarra et al. (2014 and 2016). Both studies were
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conducted in a 4 in. diameter horizontal pipe, utilizing air–liquid stratified flow. The Ibarra et al.
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(2014 and 2016) empirical correlation is selected for comparison with the developed mechanistic
models predictions, because it utilizes the same definition for the critical sand deposition velocity
as in this study.
The current study data include the air-water-solid and air–PAC/water–solid under
stratified flow. Poly Anionic Cellulose (PAC) is added to the water to increase its viscosity to 5
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cP. The experiments were conducted with three particle sizes of 45–90 µm , 125–250 µm and
425–600 µm . The liquid and gas superficial velocities are, respectively, VSL = 0.05 and 0.1 m/s
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and VSG = 3 m/s to 15.5 m/s. The experiments are conducted at low particle concentrations in the
ranges of .0000404 to 0.00404 m3/m3. Comparisons between the experimental data and the
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predictions of the current study model and Ibarra et al. (2014 and 2016) empirical correlation of
the critical sand deposition velocities are presented in Figures 8 through 13 for air–water-solid
flow, and for air–PAC/water-solid in Figures 14 to 19.
•
Air–Water–Solid Flow
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For particle size of 45–90 µm, only stationary dunes are observed for both Vsl = 0.05 and
0.1 m/s over the entire sand concentration, as shown in Figures 8 and 9, respectively. The
developed stationary dunes model predicts a fairly constant critical sand deposition velocity for
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these data. As explained before, the pilling up and collapsing mechanism exhibits a weak
function of sand concentration for the transition between Moving Dunes and Stationary Dunes.
However, the experimental results show that the critical liquid film velocity increases slightly
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with concentration. In general, reasonably good agreement is exhibited between model
predictions and the experimental data. On the other hand, Ibarra et al. (2014, 2016) correlation
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predicts a weak linear trend for the critical velocity over the entire sand concentration range. It
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over-predicts the critical velocity for Vsl = 0.1 m/s, while it is closer to the data for Vsl = 0.05 m/s.
Figure 8. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 45–90 µm at VSL = 0.05 m/s
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Figure 9. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 45–90 µm at VSL = 0.1 m/s
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Figures 10 and 11 presents the comparison for particle size of 125–250 µm, for Vsl = 0.05
and 0.1 m/s, respectively. Stationary dunes are observed only at concentrations less than 0.001
m3/m3, while for higher concentrations stationary bed occurs. As can be seen in Figure 10, the
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model for stationary dunes cannot predicts the trend of experimental data for Vsl = 0.05, showing
a flat trend. On the other hand, the model for stationary bed predicts well the experimental trend
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for the two superficial liquid velocities. Ibarra et al. (2014, 2016) correlation, again, shows a
monotonic trend over entire concentration range; it over-predicts for stationary dunes, and underpredicts for stationary bed data.
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AC
C
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Figure 10. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 125–250 µm at VSL = 0.05 m/s
Figure 11. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 125–250 µm at VSL = 0.1 m/s
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For particle size of 425–600 µm, the experimental data shows that only stationary bed is
observed for all sand concentrations. As can be seen in Figures 12 and 13, the model underpredicts the critical velocity for concentrations greater than 0.0015 m3/m3. The under-prediction
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of the model is owing to under prediction of the drag and lift forces for these concentrations. The
predictions of the model is based on a closure relationship developed for the bed height. Future
measurement of the bed height will improve the predictions of the model. Again, Ibarra et al.
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shows a linear trend, exhibiting a poor agreement with experimental model.
Figure 12. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 425–600 µm at VSL = 0.05 m/s
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Figure 13. Comparison between Experimental Data and Predicted Models for
Air–Water–Solid Flow with 425–600 µm at VSL = 0.1 m/s
Air–PAC/Water-Solid Flow
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•
The effect of liquid viscosity on the critical sand deposition velocity is presented in
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Figures 14 to 19. Note that increase in viscosity results in two competing phenomena: on the one
hand, it results in an increase in the drag force, which promotes the movement of a particle;
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however, on the other hand, it causes a reduction of the turbulent force, which promotes particle
deposition. The predictions of the new model generally show that for both Stationary Dunes and
Stationary Bed, higher liquid viscosity results in a better agreement between the model
predictions and experimental data.
For the 45–90 microns particle size, as shown in Figures 14, and 15 for Vsl = 0.05 and 0.1
m/s, respectively, only stationary bed occurs. This is owing to the effect of the viscous sublayer,
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whereby the small particles are trapped in the layer and are not exposed to the turbulence created
by the outer layer and gas-liquid interface. The model suggested by Oroskar and Turian (1980)
predicts appropriately that the turbulent force is negligible for small particle. For this case, very
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good agreement is observed between the acquired experimental data and the model predictions.
As can be seen, Ibarra et al (2014, 2016) under-predicts the critical velocity for all particle
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concentrations.
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Figure 14. Comparison between Experimental Data and Predicted Models for
Air– PAC/Water–Solid Flow with 45–90 µm at VSL = 0.05 m/s
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Figure 15. Comparison between Experimental Data and Predicted Models for
Air–PAC/Water–Solid Flow with 45–90 µm at VSL = 0.1 m/s
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The predictions of the developed models for Stationary Dunes and Stationary Bed for the
125–250 microns particle size are presented in Figures 16 and 17 for Vsl = 0.05 and 0.1 m/s,
respectively. As mentioned before, a constant critical velocity is predicted for the Stationary
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Dunes case, while the data show a slight increasing trend for concentration less than 0.001
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m3/m3. For the Stationary Bed, the model predicts the trend of the experimental data correctly.
Ibarra et al. (2014 and 2016) shows poor agreement with the stationary bed case.
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Figure 16. Comparison between Experimental Data and Predicted Models for
Air–PAC/Water–Solid Flow with 125–250 µm at VSL = 0.05 m/s
Figure 17. Comparison between Experimental Data and Predicted Models for
Air–PAC/Water–Solid Flow with 125–250 µm at VSL = 0.1 m/s
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Figures 18 and 19 presents results for the 425–600 microns particle size for Vsl = 0.05 and
0.1 m/s, respectively. As for the previous cases, a fair good agreement is observed between the
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model predictions and the experimental data for both Stationary Dunes and Stationary Bed.
The effect of viscosity on the model predictions for both Stationary Dunes and Stationary
Bed is as follows: For Stationary Dunes, the model is not sensitive to viscosity, predicting
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almost the same values for water and PAC/water flows. On the other hand, for the Stationary
Bed case, the trend of the model predictions is increasing critical sand deposition velocity with
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increasing liquid viscosity, which is in a good agreement with the experimental data collected.
Ibarra et al. (2014) model under-predicts the critical velocity over entire sand concentrations
for all three particle sizes and two superficial liquid velocities. This phenomena happens because
the correlation is developed based on experimental data collected for air-water, and the effect of
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viscosity on the critical velocity was not investigated experimentally.
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Figure 18. Comparison between Experimental Data and Predicted Models for
Air–PAC/Water–Solid Flow with 425–600 µm at VSL = 0.05 m/s
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Figure 19. Comparison between Experimental Data and Predicted Models for
Air–PAC/Water–Solid Flow with 425–600 µm at VSL = 0.1 m/s
Conclusion
Two models are developed for the prediction of the transition between Moving Dunes to
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Stationary Dunes and Moving Bed to Stationary Bed under gas-liquid stratified flow. The models
are based on the forces acting on a solid particle, such as the drag, turbulent, apparent gravity,
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van der waals and lift forces. The liquid holdup is calculated based on Taitel and Dukler (1976)
model with f I = 0 .0142 .
The model developed for Stationary Dunes is based on the pilling up and collapsing
mechanism of a dune, considering a torque balance on a particle located on the top of a dune.
The model for Stationary Bed is based on a similar torque balance applied to a particle located
on the lowest stratum of the moving bed layer. The models predict the minimum liquid film
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velocity that causes the analyzed particle to stop moving, and deposit as Stationary Bed/Dunes.
The models enable prediction of the critical sand deposition velocity and are in good
agreement when compared to the data acquired at different experimental flow conditions, such as
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different phase velocities, particle sizes, and particle concentrations. A comparison between
model predictions and the experimental data of the critical sand deposition velocity show
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absolute relative errors are 16.4% for Stationary Dunes and 12.6% for Stationary Bed.
Nomenclature
a
=
AG
=
Cross-sectional area Occupied by the Gas Phase, [ m ]
AH
=
Van Dar Waals Force Coefficient, [J]
AL
=
Cross-sectional area Occupied by the Liquid Phase, [ m ]
AP
=
Pipe Cross Sectional Area, [ m ]
APP
=
Upper Area of Particle Projected on a Plane Normal, [ ]
CD
=
Drag Coefficient, [-]
CV
=
Sand Concentration, [v/v]
dP
=
Particle Diameter, [µm]
D
=
Inside Pipe Diameter, [m]
fI
=
Interface Friction Factor, [-]
=
Kinematic Friction Coefficient, [-]
=
Drag Force, [kg.m/࢙ ]
=
Friction Force, [kg.m/࢙ ]
FL
=
Lift Force, [kg.m/࢙ ]
FT
=
Turbulent Force, [kg.m/࢙ ]
FVDW
=
Van Dar Waals Force, [kg.m/࢙ ]
FD
Ff
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2
2
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2
AC
C
fk
Leif Model Coefficient
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=
Apparent Weight Force, [kg.m/࢙ ]
g
=
Acceleration due to Gravity 9.81, [m/࢙ ]
HL
=
Liquid Holdup, [-]
k
=
Leif Model Coefficient
LD
=
Drag Force Lever, [kg.m/࢙ ]
LL
=
Lift Force Lever, [kg.m/࢙ ]
LT
=
Turbulent Force Lever, [kg.m/࢙ ]
LVDW
=
Van Dar Waals Force Lever, [kg.m/࢙ ]
LG
=
Apparent Weight Force Lever, [kg.m/࢙ ]
N
=
Weight of the Particle Itself and Other Particles in the Moving Bed Layer on
=
Solid-Liquid Density Ratio, [-]
S
=
Van Dar Waals Force Coefficient, [m]
SG
=
Gas Perimeter, [m]
SI
=
Interface Length, [m]
SL
=
Liquid Perimeter, [m]
Tnet
=
Net Torque, [kg.m.l/࢙ ]
VC
=
Critical Liquid Film Velocity, [m/s]
VLL+
EP
AC
C
VLL
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D
s
VL
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Top of It, [-]
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FG
=
Liquid Film Velocity, [m/s]
=
Local Liquid Velocity, [m/s]
=
Dimensionless Local Liquid Velocity, [-]
VM
=
Mixture Velocity, [m/s]
VM ,C
=
Critical Mixture Velocity, [m/s]
VSG
=
Superficial Gas Velocity, m/s
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VSL
=
Superficial Liquid Velocity, m/s
w
=
Factor assigned for Conversion of Turbulent Energy to Heat
x
=
Fraction of Eddies with Instantaneous Velocities Equal or Greater than the
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Terminal Velocity of the Particle, [-]
=
Distance taken from the center of the analyzed particle, [m]
y+
=
Dimensionless Distance, [-]
Greek Letters
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y
=
Pipe Inclination Angle, Radians
β
=
Particle Repose Angle, Radians
θ
=
Angle of front Dune, Radians
γ
=
Factor for Energy Dissipation, [ି ]
δ
=
Viscous Sublayer Thickness, [m]
ε
=
Pipe Roughness, [-]
µG
=
Gas Viscosity, [kg/m.s]
µL
=
Liquid Viscosity, [kg/m.s]
ρG
=
Gas Density, [kg/ ]
ρL
=
Liquid Density, [kg/ ]
ρP
=
Sand Particle Density, [kg/ ]
τI
=
Interfacial Shear Stress, [kg/m.࢙ ]
=
Wall Shear Stress, [kg/m.࢙ ]
=
Gas Phase Wall Shear Stress, [kg/m.࢙ ]
=
Liquid Phase Wall Shear Stress, [kg/m.࢙ ]
=
Liquid Kinematic Viscosity, [ /s]
τWG
τWL
υL
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AC
C
τW
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α
References
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Hydrotransport 4 (pp. A1 1-16). Banff, Alberta, Canada: BHRA Fluid Engineering, 1976.
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HIGHLIGHTS
•
Two models developed to predict the minimum liquid film velocity that causes the
•
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analyzed particle to stop moving, and deposit as Stationary Bed/Dunes.
The developed models are based on rolling mechanisms considering a torque balance
on a particle located on the top of a dune or located on the lowest stratum of the
•
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moving bed layer.
Comparison between model predictions and the experimental data of the critical sand
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deposition velocity.