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Upscaling immiscible two-phase dispersedflow in homogeneous porous media: A me-chanical equilibrium approach
O.A. Luévano-Rivas, F.J. Valdés-Parada
PII: S0009-2509(14)00718-0DOI: http://dx.doi.org/10.1016/j.ces.2014.12.004Reference: CES12028
To appear in: Chemical Engineering Science
Received date: 5 September 2014Revised date: 19 November 2014Accepted date: 1 December 2014
Cite this article as: O.A. Luévano-Rivas, F.J. Valdés-Parada, Upscalingimmiscible two-phase dispersed flow in homogeneous porous media: Amechanical equilibrium approach, Chemical Engineering Science, http://dx.doi.org/10.1016/j.ces.2014.12.004
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Upscaling immiscible two-phase dispersed flow in homogeneous
porous media: A mechanical equilibrium approach
O.A. Luevano-Rivasa, F.J. Valdes-Paradaa,∗
aDivision de Ciencias Basicas e Ingenierıa, Universidad Autonoma Metropolitana-Iztapalapa.Av. San Rafael Atlixco 186, col. Vicentina, 09340 Mexico, Mexico
Abstract
In this work, we model immiscible two-phase dispersed flow in homogeneous porous me-dia by upscaling the governing mass and momentum transport equations at the pore scaleusing the method of volume averaging. The model consists of a closed set of macroscopicequations for mass and momentum transport applicable for the dispersed and continuousphases. Furthermore, under the local mechanical equilibrium assumption, only one macro-scopic equation arises for momentum transport, which resembles an extension of Darcy’slaw; whereas for mass transport, the equilibrium model reduces to the continuity equation.These macroscopic models are written in terms of effective medium coefficients that arecomputed from solving the associated closure problems in representative regions of the porescale. After performing a parametric analysis, we observe that the magnitude of the lon-gitudinal component of the permeability-like coefficient increases with the saturation andviscosity of the dispersed phase. We validated the model by comparing the predictions ofthe permeability coefficient with experimental data available in the literature. The resultsexhibit a relative error percent that ranges from 1 % to 15 %.
Keywords: Immiscible two-phase dispersed flow, upscaling, volume averaging,permeability predictions.
∗Corresponding author. E-mail: iqfv@xanum.uam.mx
Preprint submitted to Chemical Engineering Science December 9, 2014
1. Introduction1
Immiscible dispersed flow (or emulsion flow) in porous media is important in several2
areas that include chemical, industrial, environmental science, bioenginnering, CO2 storage,3
soil remediation, enhanced-oil recovery (EOR), among others (Ouyang et al., 1995; Jain and4
Demond, 2002; Durucana et al., 2013). This type of flow in porous media, is important5
in many EOR processes where emulsions can be injected to increase the volumetric sweep6
efficiency (McAuliffe, 1973). Moreover, emulsion transport is a key component in surfactant-7
enhanced aquifer remediation technologies in subsurface zones contaminated with organic8
liquids (Jain and Demond, 2002).9
Design and improvement of processes based on emulsion flow through porous media rely10
on a better understanding of dispersed flow and its displacement mechanisms (Guillen et al.,11
2012b). Several experimental analyses have shown that the magnitude of the permeability12
coefficient may be reduced due to interception and/or deposition of the dispersed-phase13
(emulsion drops) that causes a reduction in the pore throats diameter (McAuliffe, 1973;14
Alvarado and Marsden, 1979; Soo and Radke, 1984). On the one hand, for situations in15
which the drop and pore diameter ratio is close to or larger than unity (i.e., large drops),16
it is reasonable to think interception to be relevant. On the other hand, if the ratio of drop17
and pore diameter is less than 0.2 (i.e., small drops), deposition is to be expected (Soo18
and Radke, 1984; Cobos et al., 2009). In this way, both large and small drops affect the19
permeability value; large drops block the pores, tending to reduce flow through the entire20
porous medium. In addition, several small drops, with diameters smaller than the pore21
diameter, may also be accumulated in the porous medium crevices causing the same effect22
as the large drops. Clearly, the permeability reductions depend on the volume occupied by23
the retained emulsion phase and its capacity to reduce flow (McAuliffe, 1973; Alvarado and24
Marsden, 1979; Soo and Radke, 1984; Hofman and Stein, 1991; Jain and Demond, 2002).25
Modeling single-phase flow in homogeneous porous media is usually carried out by the26
well-known Darcy’s law (Darcy, 1856). In this context, we refer to a homogeneous porous27
medium in the same sense as Quintard and Whitaker (1987), i.e., “A porous medium is28
homogeneous with respect to a given averaging volume and a given process when the effective29
transport coefficients in the volume averaged transport equations are independent of posi-30
tion”. In multiphase flow, an extension of Darcy’s law is normally used, incorporating the31
influence of each phase in a relative permeability coefficient (Dullien, 1992). In particular,32
for dispersed flow, Alvarado and Marsden (1979) presented a modified Darcy’s law model,33
which included the permeability reductions caused by partial plugging, to describe emulsion34
flow in porous media. The so-called “droplet retardation model” was originally proposed35
by McAuliffe (1973) and was mathematically described by Devereux (1974) who modified36
the classical Buckley and Leverett (1942) theory for two-phase flow in porous media that37
includes a retardation factor for the dispersed phase. In the works of Soo and Radke (1986);38
Soo et al. (1986), the filtration theory concept was used to develop a model for dilute flow39
of stable emulsion in porous media. The flow redistribution (i.e., drop capture) and large40
permeability reductions are included in this model through a filter coefficient and the effec-41
tiveness parameter of retained drops in the pore throats. The parameters were determined42
2
based on experimental data (Soo and Radke, 1984), and a redistribution parameter related43
the diversification of the flow due to the drops retained in the pores. The model was modi-44
fied by Jain and Demond (2002) to determine the hydraulic conductivity reduction caused45
by incorporating multilayer covering and viscosity variations. A Darcy-scale model was de-46
veloped by Islam and Ali (1994) for stable emulsions, including in-situ generation. The47
model was formulated in terms of conservation equations for both aqueous and oil phases,48
and coupling with the filtration model of Soo and Radke (1986); Soo et al. (1986), which49
takes into account capture mechanisms. The permeability reduction was compared with the50
experimental data of Soo and Radke (1984) obtaining good agreement. Recently, a capillary51
network model has been proposed (Cobos et al., 2009; Romero et al., 2011; Guillen et al.,52
2012b) to obtain a Darcy-scale response by using experimental pore-level flow descriptions.53
This approach incorporates flow information from a single constriction into a large capillary54
network (pores) and connecting constraints (pore throats), in order to predict the global55
permeability from the flow equation within each pore.56
Despite the progress in the study of dispersed flow in porous media, it appears that57
fundamental understanding of flow is still required in order to develop reliable models for58
this type of transport process. Evidently, the complex nature of immiscible dispersed flow59
operates at different scales that go from the pore-scale (or droplet size scale) to the Darcy-60
scale. This suggests the use of upscaling methodologies in order to derive macroscopic61
models that capture the essential features of the pore-scale by means of an averaging proce-62
dure. Upscaled models are often written in terms of effective-medium coefficients that are63
responsible of saving the essential pore-scale information. Many works have been devoted64
to carry out upscaling of immiscible two-phase flow in porous media by means of different65
approaches, such as homogenization (Auriault et al., 1989), volume averaging (Whitaker,66
1986a, 1994), and recently TCAT (thermodynamically constrained averaging theory) (Gray67
and Miller, 2014). Using the volume averaging method, Whitaker (1986a, 1994) derived68
effective-medium equations for each fluid phase. These equations were similar to Darcy’s69
law but included additional terms representing the influence of the fluid-fluid interfacial70
drag. The permeability and viscous drag coefficients involved in this approach can be com-71
puted from the solution of the associated closure problems (Whitaker, 1994; Lasseux et al.,72
1996). Later on, Lasseux et al. (1996) derived the relations between the permeability and73
viscous drag tensors and showed that both coefficients can be predicted from the same clo-74
sure problems. As indicated by Whitaker (1986a, 1994), this modeling approach involves a75
set of length-scale constraints and assumptions, some of them are summarized as follows:76
1. The characteristic length associated to the averaging domain, r0, must be much smaller77
than the characteristic length associated to the macroscale, L and, at the same time,78
r0 must be much larger than the characteristic lengths of the fluid phases, �γ and �β.79
These characteristic lengths are sketched in Fig. 1.80
2. No significant variations of the interface curvature take place within the averaging81
volume. This assumption is justified when the capillary and Bond numbers are small82
compared to one.83
3. For the closure problem solution, it was assumed that the effect of the moving contact84
3
lines can be neglected, thus restricting the model to quasi-steady flow.85
Certainly, for cases in which the coupling between both fluid phases is negligible, the model86
proposed by Whitaker reduces to Darcy’s law extension for two-phase flow, in which the87
effective permeability of each phase can be computed from the intrinsic permeability and88
the saturation (Bear and Cheng, 2010).89
For dispersed flow, the permeability cannot be determined only from the pore structure90
and the modified emulsion viscosity (Guillen et al., 2012a). Indeed, two approaches can91
be proposed for modeling dispersed flow: 1) a non-equilibrium model consisting of two92
effective-medium equations, one for each fluid phase, as Whitaker (1986a) proposed and 2)93
an equilibrium model where a single effective-medium equation (with a structure similar to94
Darcy’s law) can be used to model transport everywhere (Dullien, 1992). Both alternatives95
are discussed in this work using a volume averaging framework; however, as a first approach,96
the computations are focused on determining the effective medium coefficients associated to97
the equilibrium model.98
The paper is organized as follows: In Section 2, we present the governing equations for99
mass and momentum transport at the microscale. When applying the volume averaging100
method to these equations, we obtain the non-equilibrium model as detailed in Section101
3. To simplify this model, we adopt the local mechanical equilibrium assumption in order102
to obtain a one-equation model for describing macroscopic momentum transport in both103
fluid phases (Section 4). We clearly identify the length-scale constraints and assumptions104
supporting this macroscopic model. In Section 5, we carry out a parametric analysis of the105
permeability coefficient with the main variables of the system and we validate our predictions106
of the transport coefficients by comparison with the experimental data from Soo and Radke107
(1984) and Jain and Demond (2002). Finally, we provide the discussions and conclusions of108
our work. In addition, the details about the derivation and solution of the closure problem109
are presented in Appendix A and the details behind the local mechanical equilibrium model110
are given in Appendix B.111
2. Microscopic model112
Let us consider the immiscible flow of a dispersed phase (the γ-phase) inside a continuous113
fluid phase (the β-phase) through the pores of a homogeneous porous medium (the κ-phase).114
Both fluid phases are assumed incompressible and Newtonian, whereas the solid matrix is115
assumed to be rigid and impermeable. In addition, we constrain the analysis to situations116
in which there is only contact between two phases. In this way, the dispersed phase, which117
is regarded as a stable emulsion, is in contact with the continuous fluid phase, but not with118
the solid phase. Therefore, the governing equations for mass and momentum transport at119
the microscale are120
4
∇ · vα = 0 , in the α-phase α = β, γ (1a)
0 = −∇pα + ραg + μα∇2vα, in the α-phase α = β, γ (1b)
vβ = vγ , at the β-γ interface (1c)
nβγ ·[−pβI+ μβ
(∇vβ +∇vTβ
)]= nβγ ·
[−pγI+ μγ
(∇vγ +∇vTγ
)]+ 2σHnβγ, at the β-γ interface (1d)
vβ = 0, at the β-κ interface (1e)
In the above expressions, ρα and μα represent the density and viscosity of the α-phase121
(α = β, γ), which are assumed to be constant in the upcoming derivations. Notice that, we122
are assuming that no mass exchange is taking place between both fluid phases, hence we can123
impose continuity of the velocity as indicated in Eq. (1c). In addition, we have considered a124
jump in the momentum stress caused by purely normal capillary effects as shown in Eq. (1d).125
The interfacial tension is represented by σ and the mean curvature of the interface byH . The126
total stress tensor has been decomposed according to the Newtonian character of the fluids.127
Finally, we have imposed non-slip conditions at the boundaries between the continuous fluid128
phase and the solid in Eq. (1e). This boundary-value problem differs conceptually from129
previous studies for immiscible two-phase flow reported by Whitaker (1986a, 1994), who130
considered the contact of both fluid phases with the solid.131
3. Upscaling132
In order to obtain the effective medium equations from the microscale equations by133
means of an averaging process, we introduce a volume averaging domain, V , with norm V .134
In terms of this averaging domain, the superficial averaging operator for a given variable135
defined in either fluid phase, ψα (α = β, γ), is expressed as (Whitaker, 1999)136
〈ψα〉 = 1
V
∫Vα
ψαdV, ψ = p,v, α = β, γ (2)
where Vα is the domain occupied by the α-phase included in V . The intrinsic averaging137
operator is defined as138
〈ψα〉α =1
Vα
∫Vα
ψαdV, ψ = p,v, α = β, γ (3)
Both averaging operators are related by 〈ψα〉 = εα 〈ψα〉α, where εα is the volume fraction139
of the α-phase within the averaging domain, εα = Vα/V . The derivation of volume-averaged140
equations requires the use of the averaging theorem (Howes and Whitaker, 1985). For the141
β-phase, we have142
〈∇ψβ〉 = ∇〈ψβ〉+ 1
V
∫Aβκ
nβκψβdA+1
V
∫Aβγ
nβγψβdA (4)
5
In addition, since we have assumed that there is no contact between the dispersed phase143
and the solid, this theorem takes the following form for the γ-phase144
〈∇ψγ〉 = ∇〈ψγ〉+ 1
V
∫Aβγ
nγβψγdA (5)
The first step in the averaging process consists on applying the superficial averaging145
operators to the mass and momentum balance equations for both fluid phases. A detailed146
development of this step is available from Whitaker (1986a), here we simply provide the147
resulting expression from averaging the continuity equation, which is148
∇ · 〈vα〉 = 0, α = β, γ (6)
In order to obtain this result, it was necessary to interchange temporal differentiation with149
spatial integration, which required the use of the general transport theorem. Moreover, since150
we are limiting the analysis to situations in which there is no coalescence or shrinkage of the151
dispersed phase and the solid phase is assumed rigid, we discarded the temporal variations152
of the volume fraction in Eq. (6).153
As mentioned above, in the upscaling process, the size of the averaging domain, r0, is154
usually constrained according to (Whitaker, 1999)155
�α � r0 � L, α = β, γ (7)
In this relation, �α represents the characteristic length of the α-phase at the microscale and156
the system macroscopic length is denoted by L, as sketched in Fig. 1.157
Furthermore, the resulting expression from the application of the superficial averaging158
theorem to the momentum balance equation for the β-phase is (see Whitaker, 1986a, for159
details)160
0 = −∇〈pβ〉β+ρβg+μβ∇2 〈vβ〉β+ 1
Vβ
∫Aβκ
nβκ·[−pβI+ μβ∇vβ] dA+1
Vβ
∫Aβγ
nβγ ·[−pβI+ μβ∇vβ ] dA
(8a)and for the γ-phase is161
0 = −∇〈pγ〉γ + ργg + μγ∇2 〈vγ〉γ + 1
Vγ
∫Aβγ
nγβ · [−pγI + μγ∇vγ] dA (8b)
In writing Eqs. (8), the spatial variations of the physical properties (density and viscosity) of162
the fluid-phases in the averaging domain have been neglected. In addition, we have taken into163
account the non-slip condition in the derivation of these equations, as well as the separation164
of characteristic lengths expressed in (7). Furthermore, since we are directing the analysis165
to the homogeneous regions of a porous medium, we have regarded the volume fractions as166
6
constants. Finally, we have expressed the result in terms of both intrinsic averaged properties167
and their spatial deviations, the latter are defined from the decomposition (Gray, 1975)168
ψα = ψα + 〈ψα〉α (9)
The process of determining the functionality of the spatial deviations in terms of the169
corresponding averaged quantities is known as closure. The development of the formal170
solution of the closure problem is quite extensive and the details are available in Appendix171
A. The formal solutions of the closure problems for the deviations variables can be expressed172
as follows173
vα = Aα · 〈vβ〉β + Aαλ ·(〈vβ〉β − 〈vγ〉γ
)+ dα
(〈pβ〉β − 〈pγ〉γ
)+ fα, α, λ = β, γ, α �= λ
(10a)
pα = μα
[aα · 〈vβ〉β + aαλ ·
(〈vβ〉β − 〈vγ〉γ
)+ sα
(〈pβ〉β − 〈pγ〉γ
)+ ϕα
](10b)
where Aα, Aαλ, aα, aαλ, dα, fα, sα and ϕα (α = β, γ), are the so-called closure variables,174
which arise from the non-homogeneous terms involved in the boundary-value problem for175
the deviations variables. The closure variables solve the boundary-value problem given in176
Eqs. (A.8). The derivation of this problem requires considering the length-scale constraint177
given in (7) (see Appendix A for details).178
Substitution of eqs. (10a) and (10b) into eqs. (8a) and (8b) gives rise to the non-equilibrium (NE) model for the β-phase:
0 = −∇〈pβ〉β + ρβg + μβ∇2 〈vβ〉β + μβεβ(−Kne
ββ
)−1 · 〈vβ〉β + μβKneβγ ·(〈vβ〉β − 〈vγ〉γ
)+
μβuβ
(〈pβ〉β − 〈pγ〉γ
)+ μβhβ (11)
here, the effective-medium coefficients are defined as follows179
−εβ(Kne
ββ
)−1=
1
Vβ
∫Aβκ
nβκ · [−aβI+∇Aβ] dA+1
Vβ
∫Aβγ
nβγ · [−aβI+∇Aβ] dA (12a)
180
Kneβγ =
1
Vβ
∫Aβκ
nβκ · [−aβγI+∇Aβγ ] dA+1
Vβ
∫Aβγ
nβγ · [−aβγI+∇Aβγ ] dA (12b)
181
uβ =1
Vβ
∫Aβκ
nβκ · [−sβI+∇dβ] dA+1
Vβ
∫Aβγ
nβγ · [−sβI+∇dβ] dA (12c)
182
hβ =1
Vβ
∫Aβκ
nβκ · [−ϕβI+∇fβ] dA+1
Vβ
∫Aβγ
nβγ · [−ϕβI+∇fβ] dA (12d)
183
7
The closed form of the upscaled non-equilibrium model for the γ-phase is
0 = −∇〈pγ〉γ + ργg + μγ∇2 〈vγ〉γ + μγεγ(−Kne
γβ
)−1 · 〈vβ〉β + μγKneγγ ·(〈vβ〉β − 〈vγ〉γ
)+ μγuγ
(〈pβ〉β − 〈pγ〉γ
)+ μγhγ (13)
in this case, the effective-medium coefficients are defined as follows184
−εγ(Kne
γβ
)−1=
1
Vγ
∫Aβγ
nγβ · [−aγI+∇Aγ] dA (14a)
185
Kneγγ =
1
Vγ
∫Aβγ
nγβ · [−aγβI+∇Aγβ] dA (14b)
186
uγ =1
Vγ
∫Aβγ
nγβ · [−sγI+∇dγ] dA (14c)
187
hγ =1
Vγ
∫Aβγ
nγβ · [−ϕγI+∇fγ] dA (14d)
188
In this model, we notice that the first three terms in eqs. (11) and (13) are volume-189
averaged versions of the micro-scale Stokes’ equation and the rest are the result of the190
upscaling process. Regarding this upscaled model, the following comments are in order:191
• The main contributions from microscopic momentum transport (represented by the192
closure variables) are captured in the effective-medium coefficients, which are defined193
in terms of integrals (i.e., filters) of the closure variables. These coefficients are: 1) The194
permeability tensors Kneββ and Kne
γβ, which are defined in terms of the closure variables195
aα and Aα (α = β, γ). These closure variables arise from solving a closure problem196
in which the only source is located at the β − κ interface, just like in the case of197
the permeability tensor in Darcy’s law (see eqs. (4.2-27) in Whitaker, 1999). 2) The198
tensors Kneβγ and Kne
γγ , which may be interpreted as interfacial momentum transport199
coefficients, because they are defined in terms of the closure variables aαλ and Aαλ200
(α, λ = β, γ and α �= λ). These closure variables arise from solving a closure problem201
in which the source term is located in the velocity boundary condition at the fluid-202
fluid interface. 3) The vectors uα (α = β, γ), are similar to the previous ones but they203
account for the microscopic differences in stress at the fluid-fluid interface. 4) The204
vectors hα (α = β, γ), are the result of considering the capillary effects of curvature205
and superficial tension in the closure problems.206
• It is important to point out that the validity of eqs. (11) and (13) is bounded by207
the length-scale constraint given in (7). In addition, the application of the model is208
limited to non-coalescing emulsions, for this reason the flow is assumed quasi-static,209
8
and the volume fractions for the β and γ-phases are regarded as given parameters.210
This means that the predictions of the effective-medium coefficients in this model211
(or in the equilibrium model shown below) are only functions of the porosity and212
the saturation. This set of constraints and assumptions can be visualized as scaling213
postulates as suggested by Wood and Valdes-Parada (2013).214
• It should be stressed that the model derived here is different from the model derived215
by Whitaker (1986a) because of the last two terms in eqs. (11) and (13). Indeed, the216
pressure difference in the first term can be related to the average curvature of the217
fluid-fluid interface, according to (Whitaker, 1986a)218
−(〈pβ〉β − 〈pγ〉γ
)= 2σ 〈H〉βγ (15)
where the average curvature is defined as219
〈H〉βγ =1
Aβγ
∫Aβγ
H dA (16)
It should be stressed that Eq. (15) is valid under the capillary restriction, Ca � 1220
(Whitaker, 1994). Here the Capillary number is defined as Ca = μ〈v〉/σ, with μ〈v〉221
representing the magnitude of the largest of μα〈vα〉α (α = β, γ). Furthermore, in order222
for the mean curvature to undergo negligible variations within the averaging volume,223
it is necessary to impose that (Whitaker, 1994)224
Bo =(ρβ − ργ)g�
2
σ� 1 (17)
with Bo denoting the Bond number and � is a characteristic length representing the225
largest of �α (α = β, γ). Under these conditions, the contributions of these two terms226
become negligible as noted by Whitaker (1986a) and the non-equilibrium model can227
be arranged as228
0 = −∇〈pβ〉β+ρβg+μβ∇2 〈vβ〉β+μβ
[εβ(Kne
ββ
)−1+Kne
βγ
]·〈vβ〉β−μβK
neβγ ·〈vγ〉γ (18a)
229
0 = −∇〈pγ〉γ+ργg+μγ∇2 〈vγ〉γ+μγ
[εγ(Kne
γβ
)−1+Kne
γγ
]·〈vβ〉β−μγK
neγγ ·〈vγ〉γ (18b)
In order to recover Whitaker’s result, the following definitions are introduced[εβ(Kne
ββ
)−1+Kβγ
ne]=− εβK
−1β (19a)
−Kneβγ = εγK
−1β ·Kβγ (19b)[
εγ(Kne
γβ
)−1+Kne
γγ
]= εβK
−1γ ·Kγβ (19c)
−Kneγγ = − εγK
−1γ (19d)
9
In this way, after some manipulations, eqs. (18) can be expressed as230
εβ 〈vβ〉β = −Kβ
μβ
(∇〈pβ〉β + ρβg
)+Kβ∇2 〈vβ〉β +Kβγ · εγ 〈vγ〉γ (20a)
231
εγ 〈vγ〉γ = −Kγ
μγ(∇〈pγ〉γ + ργg) +Kγ∇2 〈vγ〉γ +Kγβ · εβ 〈vβ〉β (20b)
232
These equations correspond to the modified version of Darcy’s law with the Brinkman233
correction and the viscous drag indicated originally in previous works (Whitaker,234
1986a, 1994; Lasseux et al., 1996).235
Finally, it is worth remarking that this work is restricted to cases in which the γ-phase is236
dispersed in the β-phase and there is no triple-phase contact. This means that the predictions237
of the transport coefficients provided below are not extensible to the situations studied by238
Whitaker (1986a, 1994); Lasseux et al. (1996). However, to the best of our knowledge,239
no numerical solution to the closure problems stated in these works has been reported in240
the literature. We believe that the computations presented in the following paragraphs241
for dispersed flow in the local mechanical equilibrium model constitute a relevant advance242
towards the solution of the closure problems presented by Lasseux et al. (1996).243
4. Local mechanical equilibrium model244
The derivations presented in the previous section consist in two effective-medium equa-245
tions for each fluid phase in the system (eqs. 11 and 13). However, previous works for246
studying heat and mass transport in multiphase systems have suggested the use of local247
equilibrium models, which rely on a single weighted-averaged temperature or concentration248
to provide a reasonable description of the whole transport process (Whitaker, 1991; Quin-249
tard and Whitaker, 1995; Ochoa-Tapia et al., 1986; Wood and Whitaker, 1998). Certainly,250
this modeling approach is simpler and thus more attractive than the non-equilibrium model.251
However, the use of equilibrium models requires imposing additional assumptions aside from252
those involved in the averaging process. For situations in which these constraints are met,253
the comparison of the predictions from the equilibrium model, with those resulting from254
laboratory or numerical experiments yields good agreement (Quintard and Whitaker, 1993,255
1995). Furthermore, the use of equilibrium models is not restricted to the bulk of porous256
media and has been recently extended to the fluid-porous medium boundary as shown by257
Aguilar-Madera et al. (2011). In that work, the equilibrium model was shown to satis-258
factorily reproduce the predictions from both the non-equilibrium model and from direct259
numerical simulations. For momentum transport, equilibrium models have been proposed260
for the study of heterogeneous porous media as shown by Quintard and Whitaker (1988).261
Motivated from the above, in this work we propose a local mechanical equilibrium (LME)262
approach for modeling dispersed flow in homogeneous porous media. In this model, the263
10
dependent variables are written in terms of the following intrinsic average (hereafter denoted264
as the equilibrium average)265
〈ψ〉 = 1
Vf
∫Vf
ψdV =1
Vf
∫Vβ
ψβdV +1
Vf
∫Vγ
ψγdV, ψ = v, p (21)
here Vf = Vβ +Vγ, is the volume occupied by the fluid phases. At this point, it is opportune266
to define the porosity as ε = Vf/V and the volume fractions for each phase as εα = Vα/V ,267
so that Eq. (21) can be rearranged as268
ε 〈ψ〉 = εβ 〈ψβ〉β + εγ 〈ψγ〉γ = 〈ψβ〉+ 〈ψγ〉 (22)
On the basis of this definition, we may add the upscaled continuity equations for each269
phase [eqs. (6)] and obtain, without any further simplification, the following expression for270
the equilibrium mass transport model271
∇ · ε〈v〉 = 0 (23)
However, for momentum transport, the derivations of the equilibrium model is not as272
straightforward. We will follow a procedure previously used for studying heat transfer in273
porous media (see Whitaker, 1999, Chap. 2), as a first step towards this derivation, it is274
convenient to decompose the intrinsic averages of each phase in terms of the equilibrium275
average, 〈ψ〉, and the macroscopic deviations, ψ, as follows276
〈ψα〉α = 〈ψ〉+ ψα, ψ = v, p, α = β, γ (24)
In this way, we can derive the governing equation for 〈ψ〉 by substituting Eq. (24) into277
the non equilibrium model (eqs. (11) and (13)) and combine the resulting expressions278
accordingly to obtain279
0 = −∇〈p〉+ 〈ρ〉 g + 〈μ〉∇2 〈v〉 − μβ (Ke)−1 · ε 〈v〉+ 〈μ〉he +Φ (25)
here we introduced the definitions280
〈ρ〉 = Sβρβ + Sγργ (26a)
281
〈μ〉 = Sβμβ + Sγμγ (26b)282
μβ (Ke)−1 = Sβμβ
(Kne
ββ
)−1+ Sγμγ
(Kne
γβ
)−1(26c)
283
μβhe = Sβμβhβ + Sγμγhγ (26d)
In the above expressions, we used Sα = εα/ε, α = β, γ to represent the saturation for a284
given porosity and volume fraction of the α-phase. The term Φ in Eq. (25) includes all the285
terms involving the macroscopic deviations, ψα,286
11
Φ = ε−1 (μβ − μγ)SβSγ∇2(〈vβ〉β − 〈vγ〉γ
)+(μβSβK
neβγ + μγSγK
neγγ
) · (〈vβ〉β − 〈vγ〉γ)
(−μβSβ
(Kne
ββ
)−1+ μγSγ
(Kne
γβ
)−1)SβSγ ·
(〈vβ〉β − 〈vγ〉γ
)+
(μβSβuβ + μγSγuγ) ·(〈pβ〉β − 〈pγ〉γ
)(27)
Under the assumption of local mechanical equilibrium, we expect that Φ can be assumed287
negligible with respect to the other terms in Eq. (25). The assumptions and length-scale288
constraints required to determine the validity of the local mechanical equilibrium model are289
addressed in Appendix B. These conditions can be loosely summarized as follows:290
• One fluid phase is in much larger proportion than the other, for example, εγ � εβ.291
• The physical properties of both phases are alike, i.e., ρβ ∼ ργ and μβ ∼ μγ.292
• There is a disparity of characteristic lengths of the type �� L.293
Under the local mechanical equilibrium assumption, we may drop the Φ term in Eq. (25)294
and simplify it to obtain the following expression295
0 = −∇〈p〉+ 〈ρ〉 g + 〈μ〉∇2 〈v〉 − μβ (Ke)−1 · ε 〈v〉+ 〈μ〉he (28)
If the LME assumption is valid, and it is applied to the closure problem derived inAppendix A, the formal solution for the deviations variables given by Eq. (10) reduces to
vα = Aα · 〈v〉+ fα, α, λ = β, γ, α �= λ (29a)
pα = μα [aα · 〈v〉+ ϕα] (29b)
and the associated boundary-value problems are Problems I and IV from Table A.2, where296
the only sources will be 〈v〉 and H , respectively. To close the model of the LME model we297
have to solve these boundary value problems in order to compute the fields of the closure298
variables and thus obtain predictions of the effective tensors and vectors. The expressions299
for Ke and he in terms of closure variables are given in eqs. (A.11) and (A.12). The closure300
problems are solved in the unit cell for dispersed flow sketched in Fig. A.1. However, as301
mentioned above, in order to neglect significant variations of the interfacial curvature, within302
the averaging volume, it is necessary to impose that Ca� 1 and Bo� 1. As consequence,303
we have that304
〈μ〉he � μβ (Ke)−1 · ε 〈v〉 (30)
and thus, Eq. (28) reduces to305
ε 〈v〉 = −Ke
μβ· (∇〈p〉 − 〈ρ〉g) + 〈μ〉
μβKe · ∇2 〈v〉 (31)
12
This result can be further modified if the definition of Ke is related to the intrinsic306
permeability and a correction factor . We can introduce a new definition for the effective307
coefficient in terms of these contributions as308
(Ke)−1 = K−1 · (I+Km) (32)
where K is the intrinsic permeability coefficient defined by Whitaker (see Eq. (4.2-32) in309
Whitaker, 1999) and Km is the correction factor that takes into account the effect of the310
dispersed phase. As explained by Whitaker (1999), in order to compute K, it is necessary311
to solve a Stokes-like problem in a periodic unit cell (see eqs. (4.2-37) in Whitaker, 1999).312
Furthermore, in order to compute the values of Km, it is necessary to solve the closure313
problems defined in Appendix A. This correction factor is only influenced by the viscosity314
ratio and by the volume fraction occupied by each phase in the system. Examples of the315
solution of the closure problems are provided in the following section along with a parametric316
study of the functionality of the effective medium coefficients.317
Substitution of Eq. (32) into Eq. (31), gives rise to the following form of the upscaled318
model that resembles to an extension of the Darcy-Brinkman model319
ε 〈v〉 = − K
μβ· (∇〈p〉 − 〈ρ〉 g) + 〈μ〉
μβK · ∇2 〈v〉 −Km · ε 〈v〉 (33)
In this expression, the first term on the right-hand side represents the Darcy term,320
the second one is the Brinkman correction term and finally the effect of the dispersed γ-321
phase is accounted in the last term. As explained by Ochoa-Tapia and Whitaker (1995),322
the Brinkman correction term is crucial in the study of transport phenomena near the323
boundaries of a porous medium. However, in the porous medium bulk, this term can be324
safely discarded. Under these conditions, Eq. (33) can be reduced to325
ε 〈v〉 = − K
μβ· (∇〈p〉 − 〈ρ〉 g)−Km · ε 〈v〉 (34)
Or, in terms of Ke,326
ε 〈v〉 = −Ke
μβ
· (∇〈p〉 − 〈ρ〉 g) (35)
Notice that, although the structure of the above expression resembles to Darcy’s law, the ef-327
fective medium coefficient, Ke, does not, in general, correspond to the intrinsic permeability,328
K. As a matter of fact, from Eq. (32), it can be deduced that (Ke)−1 ≈ K−1, only for condi-329
tions in which Km � I. These conditions will be discussed in the following paragraphs. As330
mentioned in the introduction, Darcy’s law has been largely used in the literature to model331
multiphase flow in porous media (Alvarado and Marsden, 1979; Soo and Radke, 1984; Hof-332
man and Stein, 1991; Islam and Ali, 1994; Jain and Demond, 2002; Romero et al., 2011;333
Nogueira et al., 2013). The effective-medium coefficient involved in this upscaled model is334
usually predicted from best-fits of experimental data from emulsion flow in porous media335
and, more recently, in microchannels flow (e.g. Cobos et al., 2009). In this work, Ke is336
predicted from the solution of the associated closure problems in a representative unit cell,337
as detailed below.338
13
5. Prediction of the effective coefficients339
5.1. Parametric analysis340
In this section, we analyze the parametric dependence of the effective transport coef-341
ficients involved in the LME model with the main degrees of freedom. These are: the342
saturation (Sα = Vα/Vf = εα/ε), the viscosity ratio ν = μβ/μγ and the void fraction ε.343
The solution of the closure problems and the computations of the effective parameters were344
performed using the commercial finite element solver Comsol MultiphysicsTM (version 4.3a).345
The default element types and solvers were used in all simulations. In addition, adaptive346
mesh refinements algorithms were applied in order to ensure that the results were indepen-347
dent of the computational elements. All closure problems were solved in the 2D unit cells348
illustrated in Fig. A.1. In this model of the microscale geometry, the γ-phase is represented349
by a series of circular particles with five different diameters, rγi, i = 1, · · · , 5 (details are350
presented in Appendix A). Certainly, we are assuming flow conditions in which the droplets351
do not modify their shape, size and position. The latter was conveniently fixed in order352
to satisfy the saturation values. The κ-phase is represented by a circular particle with the353
radius determined by the value of the void fraction; rκ =√(1− ε) /π. The closure prob-354
lem solution was carried out in order to obtain the longitudinal component of the effective355
transport coefficients (i.e., the x-direction). Examples of the fields of longitudinal closure356
variables (Aα)xx , α = β, γ are presented in Fig. 2.357
Once the solution fields of the closure variables are obtained, they are substituted into358
Eq. (A.11) that defines the effective coefficient for LEM model given in Eq. (35). In Fig. 3359
we show the dependence of the longitudinal component of the effective coefficient (Ke = Kexx)360
involved in the LEM model, with the main parameters (ε, ν and Sβ). Analyzing these results,361
the following comments are in order:362
• As expected from previous studies about one-phase flow in porous media, Ke increases363
with the void fraction. As a matter of fact, for the case in which ν = 1, the results364
reproduce those from the intrinsic permeability. In our computations we had to limit365
the porosity values to be larger than 0.5, otherwise the largest drops tend to have a366
diameter that is almost equal to the pore diameter.367
• We observe in Fig. 3 that, if the volume in the pore is occupied by the continuous phase368
in a minor proportion with respect to the dispersed phase (Sβ = 0.35), the predictions369
are more sensitive to changes with ν than when the pore volume is occupied in major370
proportion by the continuous phase (Sβ = 0.8). Regarding the influence of ν, we371
note that Ke increases with this parameter. This is to be expected from the previous372
analysis of the fields in Fig. 2; especially as Sβ decreases, which translates in a larger373
volume fraction of the dispersed phase.374
• In Figs. 3a,b, we observe that, for ν > 1 (μβ > μγ), the values of Ke are larger than375
the ones corresponding to the intrinsic permeability given by ν = 1. Furthermore,376
for ν < 1 (μβ < μγ), the predictions of Ke are smaller than K, and Ke decreases as ν377
decreases (Figs. 3c,d).378
14
It should be noted that the analysis of the results provided above does not show very379
clearly the influence of each phase in the effective medium coefficient Ke. To gain a better380
understanding of the role played by the continuous and the dispersed phases, it is convenient381
to direct the attention to Eq. (32), in which Ke is expressed in function of the intrinsic382
permeability and a correction factor Km. From this expression, we observe on the one hand383
that if Km > 0, it turns out that Ke < K, which means that the dispersed phase hinders384
the overall momentum transport. On the other hand, for situations in which −1 < Km < 0,385
it results in the effective coefficient being larger than the intrinsic permeability, i.e., an386
enhanced momentum transport.387
Using the solution fields of the closure involved in the computation of Ke (eqs. A.8a -388
A.8i) and solving the corresponding boundary value problem to obtain K (see Eq. (4.2-32)389
in Whitaker, 1999) in the same unit cell shown in Fig A.1, we can compute Km = (Km)xx.390
The predictions of Km are plotted in Fig. 4 as a function of ε for different values of ν taking391
Sβ = 0.8. We provide the following comments regarding the results shown in the Fig. 4:392
• For ν > 1, the negative values of Km results in Ke > K. Therefore, as the ν increases,393
the effective coefficient Ke increases and, as consequence, the global dispersed flow394
is enhanced by the presence of the dispersed γ-phase. Although the results are only395
presented for one saturation value, from the results in Fig. 3, it is appealing to think396
that if Sβ increases, the volume of the dispersed phase decreases and the enhanced397
effect is reduced. At this point, it is worth recalling that the assumptions adopted so398
far lead to neglecting the influence of the interfacial tension between the continuous399
and dispersed phases, thus the viscosity ratio and the volume occupied by each phase400
are the main parameters that determine the values of the correction factor.401
• In the case of ν = 1, the effect of the γ-phase over the effective coefficient can be402
neglected because Km � I, which results in values of Ke ≈ K. The presence of the403
both immiscible phases in the homogeneous porous media is similar to one-phase flow.404
• In contrast, the values Km are positive for ν < 1, therefore Ke < K. This results suggest405
the global flow is detracted by the presence of the dispersed fluid where the γ-phase406
is acting like “drag particles”. Therefore, reduction the Sβ increase the volume of this407
drag particles as consequence the drag will be increased.408
To conclude this section, we provide a validation of the effective coefficient predictions409
with experimental data obtained from the literature. This analysis is presented in the fol-410
lowing paragraphs.411
5.2. Comparison with experiments412
In this section, the prediction of the effective coefficient for the LME model, Ke, are413
compared with the experimental data reported by Soo and Radke (1984); Jain and Demond414
(2002). The experimental data reported by Soo and Radke (1984) were obtained in a system415
where a dilute emulsion of known concentration and drop-size distribution is slowly flowed416
to a sandpack of known pore size distribution and permeability under a constant volumetric417
15
flow rate. The permeability reduction is determined by changes in the pressure drop and418
the reduction of drops concentration after the flush. The conditions for several experiments419
reported by Soo and Radke (1984) are presented in Table 1.420
The effective coefficient for the LME model is computed using the solution of the closure421
problem in the unit cell shown in Fig. 5 that attempts to capture the essential geometric422
information obtained by the experimental system described above. In Fig. 5, the sand grain423
of the porous media are represented by circles with radius: rκ =√
(1− ε)/2π and the pore424
diameter is: dp =(√
1/2)�c − 2rκ. For given values of Sγ and ε, the number of circles425
needed to represent the dispersed γ-phase, Nγ , is computed by: Nγ = Sγε/ (πrγ) using the426
data in Table 1. The localization of the circles was chosen to be near the pore throats on427
the basis of previous studies (Soo and Radke, 1984) that concluded that the dispersed phase428
reduces the pore throats diameter by the deposition and interception of the droplets. It429
should be stressed that in the experiments by Soo and Radke (1984), the droplets were not430
monodispersed. However, the droplets sizes did not exhibit large deviations from the average431
drop size as shown in Fig. 3 of Soo and Radke (1984). For this reason, the droplet size, 2rγ,432
used in the unit cell shown in Fig. 5 corresponded to the average droplet size reported by433
Soo and Radke (1984). In addition, note that, in all the experimental data studied here, the434
values of 2rγ were smaller than the pore diameter in the unit cell, dp, as shown in Table 1.435
In Fig. 6 we present the comparison between the experimental data of Soo and Radke436
(1984) and the predicted coefficients for the LME model obtained by the closure problem437
solution illustrated in Fig. 5. The predictions were compared with several emulsified systems,438
which included variations in the viscosity of γ - phase, as well as variations in the pore439
diameter and drop size, as shown in Table 1. To have a more qualitative perspective of the440
predictive capabilites of the LME model, in Fig. 6b we plot the computed relative error441
percent between the theoretical predictions and the experimental data. We observe that,442
except for the last experimental value in experiment 1, all the results exhibit a relative error443
percent that is below 7%, which may be considered acceptable in many situations. It should444
be stressed that the predictions of the experimental data showed a strong dependency with445
the geometric parameters and, for this reason, the largest errors were found for the higher446
values of 1− Sβ.447
The predictions of the effective-medium coefficients involved in the LME model are com-448
pared with the experimental data reported by Jain and Demond (2002) in Fig. 7. The449
experimental methodology is essentially the same described above and the parameters used450
for the simulations are provided in Table 1. In this case, the range of saturation values451
is larger and, not surprisingly, the relative error percent between theory and experiments452
increases up to 15 % for the smallest value of Sβ . This increase of the error percent with453
1−Sβ can be associated with the increases in the number of particles necessary to complete454
the saturation and to the set of assumptions involved in the derivation of the model, among455
which is the assumption that there is no interaction between the dispersed phase and the456
solid. In addition, more elaborated geometries can be used in the unit cell, which may457
provide better agreement with the experimental data. However, we believe that the simple458
geometries used in this work, as a first approach, yield to reasonable agreement with the459
16
experimental data.460
6. Discussion and conclusions461
In this work, we applied the method of volume averaging to obtain an upscaled model462
for modeling immiscible two-phase dispersed flow in homogeneous porous media. We have463
considered the conditions of stable-steady emulsion flow in the microscale model. We ob-464
tained closed macroscopic mass and momentum transport equations that, under the local465
mechanical equilibrium hypothesis can be applied to both continuous and dispersed phases.466
In this model, the momentum transport equation is written in terms of effective-medium467
coefficients that incorporate the microscopic geometry effects and the momentum transport468
between both phases. These coefficients can be predicted from the solution of the associated469
closure problem in representative periodic unit cells that capture the essential features of470
the pores scale. In this way, we found conditions in which the presence of the dispersed471
phase enhances or hinders the macroscopic momentum transport.472
It should be noted that the local mechanical equilibrium, despite being a relatively473
simple approach, contains more restrictions than its non-equilibrium counterpart. The non-474
equilibrium model is in agreement with previous applications of the volume averaging method475
by Whitaker (1986b), where the resulting model is a set of macroscopic equations, one for476
each phase, that resemble Darcy’s law with an extra term that is related to the interaction477
between both phases (see eqs. 20). On the other hand, the equilibrium model, as expressed478
in Eq. (35), can be written in a way that resembles Darcy’s law. However, the coefficient Ke479
is not intrinsic, in general, because it depends of the phases interaction. For this reason, it is480
more convenient to use Eq. (32) and express the equilibrium model in the form given in Eq.481
(34), which contains the permeability tensor K involved in one-phase flow and a correction482
factor accounting for the interaction between the phases. Indeed, more research is needed483
and an exhaustive comparison of the equilibrium and non equilibrium formulations should484
be addressed in a future work.485
The results of our parametric analysis evidence that, for conditions in which μβ > μγ486
(i.e., ν > 1) momentum transport is enhanced and thus Km < 0 and the opposite is true.487
This observation is relevant because in many EOR or soil remediation applications (Ouyang488
et al., 1995; Jain and Demond, 2002; McAuliffe, 1973) it is desirable to enhance global flow.489
In this way, for conditions in which the assumptions supporting the LME model, one may490
predict operational conditions in which the transport can be enhanced and thus look for491
optimal operation conditions.492
The relatively good agreement between the theoretical predictions and experimental493
data encourages us to believe that the LME approach may be reasonable in applications in494
which the saturation Sβ is large. We attribute the largest deviations between theory and495
experiments to the geometrical limitations in the unit cell used here and to the length scale496
constraints and assumptions involved in the derivation of the model. Briefly, we assumed497
that there is no contact between the dispersed phase and the solid phase, that the influences498
of curvature and interfacial tension are negligible and that there should be a separation499
of characteristic scales between the pore scale and the macroscale. In future works we500
17
shall expand the range of applicability of the model derived here by relaxing some of these501
assumptions. Nevertheless, the relative error in most of the results remained below 10%502
with respect to experimental data. We can thus conclude that, in general, the predictions503
exhibit acceptable agreement with the experimental data examined here.504
In future works we will investigate the use of more complicated unit cells, in particular, it505
would be enlightening to use three-dimensional domains with more realistic representations506
of the porous matrix and of the dispersed phase location and size distribution. Another507
topic that should be investigated is the possibility to consider droplets’ coalescence and508
their interaction with the solid phase. These and other extensions of the current research509
will be explored in future work.510
Appendix A. Closure problem for NLME511
The objective in this section is to present the details in relation with the functionality of512
the spatial deviations and the average quantities in order to close the macroscopic model.513
From Eq. (9), we have that the spatial deviations of any quantity are: ψα = ψα − 〈ψα〉α.514
Directing the attention to mass transport, it is convenient to write Eq. (6) in terms of515
intrinsic averages as follows516
∇ · 〈vα〉α = 0, α = β, γ (A.1)
here we have taken into account the assumption that the porous medium is homogeneous517
and, consequently, εα is treated as a constant. Subtracting Eq. (A.1) to Eq. (1a), gives rise518
to519
∇ · vα = 0 in the α-phase, α = β, γ (A.2)
For momentum transport, the governing equations for the deviations result from sub-520
tracting eqs. (8) and (1b) and can be written as521
0 = −∇pβ + μβ∇2vβ − 1
Vβ
∫Aβκ
nβκ · [−pβI+ μβ∇vβ ] dA− 1
Vβ
∫Aβγ
nβγ · [−pβI+ μβ∇vβ ] dA
in the β-phase (A.3a)
522
0 = −∇pγ + μγ∇2vγ − 1
Vγ
∫Aβγ
nγβ · [−pγI+ μγ∇vγ ] dA, in the γ-phase (A.3b)
523
The closure problem is completed by the following interfacial boundary conditions that524
arise from substituting the spatial decompositions for the pressure and velocity into eqs.525
(1c)-(1e)526
18
vβ = vγ −(〈vβ〉β − 〈vγ〉γ
), at the β-γ interface (A.4a)
nβγ ·[−pβI+ μβ
(∇vβ +∇vTβ
)]=nβγ ·
[−pγI+ μγ
(∇vγ +∇vTγ
)]+ nβγ
(〈pβ〉β − 〈pγ〉γ
)+ 2σHnβγ, at the β-γ interface
(A.4b)
vβ = −〈vβ〉β , at the β-κ interface (A.4c)
Notice that, in Eq. (A.4b) we have followed Whitaker (1994) and neglected the contribution527
of the macroscopic viscous terms. This assumption is justified by the length-scale constraint528
�α � L (α = β, γ). In addition, the fields of the deviations are bounded by the following529
average constraint530 ⟨ψα
⟩α= 0, ψ = p,v, α = β, γ (A.5)
Finally, following previous approaches (e.g., Whitaker, 1986a), the closure problem is531
solved in a periodic representative domain of the microscale (i.e., a unit cell). This motivates532
imposing the following boundary conditions at the entrances and exits of the unit cell.533
ψα (r+ li) = ψα (r) , ψ = p,v; α = β, γ; i = 1, 2, 3 (A.6)
From this statement of the closure problem, we identify the sources 〈vβ〉β,(〈vβ〉β − 〈vγ〉γ
),(
〈pβ〉β − 〈pγ〉γ)and 2σH . Given the linear nature of this boundary-value problem, we can
propose a formal solution in terms of the sources as follows
vα = Aα · 〈vβ〉β + Aαλ ·(〈vβ〉β − 〈vγ〉γ
)+ dα
(〈pβ〉β − 〈pγ〉γ
)+ fα, α, λ = β, γ, α �= λ
(A.7a)
pα = μα
[aα · 〈vβ〉β + aαλ ·
(〈vβ〉β − 〈vγ〉γ
)+ sα
(〈pβ〉β − 〈pγ〉γ
)+ ϕα
](A.7b)
534
In equations (A.7a) and (A.7b), the variables Aα, Aαλ, aα, aαλ, dα, fα, sα and ϕα are535
known as the closure variables. Indeed, one may rearrange the first two terms on the right536
hand side of the above expressions to be proportional to the intrinsic averaged velocity in each537
phase; however, we find it more convenient to express the formal closure problem solution538
in its current form because, under equilibrium conditions, the terms involving differences539
of volume averaged quantities are null and eqs. (A.7) reduce to eqs. (29). Each closure540
variable can be conceived as a mapping function of a source onto the deviations fields. In541
this way, for example, dα maps the difference of the intrinsic averaged pressures onto vα;542
whereas fα and ϕα map H and μαH onto vα and pα, respectively.543
Substitution of the formal solution given by eqs. (A.7) into eqs. (A.2)-(A.5) and (A.6),544
gives rise to four closure problems. For the sake of brevity in presentation, these problems545
are compacted into the following one546
19
∇ · Zβ = 0 in the β-phase (A.8a)
−∇ζβ +∇2 Zβ = Δβ in the β-phase (A.8b)
Zβ = Zγ +ΔIβγ , at the β-γ interface (A.8c)
μβ
[−ζβI+(∇Zβ +∇ZT
β
)] · nβγ = μγ
[−ζγI+(∇Zγ +∇ZT
γ
)] · nβγ
+ΔIIβγ , at the β-γ interface (A.8d)
Zβ = Δβκ, at the β-κ interface (A.8e)
∇ · Zγ = 0 in the γ-phase (A.8f)
−∇ζβ +∇2 Zβ = Δγ in the γ-phase (A.8g)
Zα (r+ li) = Zα (r) , i = 1, 2, 3 (A.8h)
〈Zα〉α = 0 (A.8i)
where Zα and ζα represent the closure variables and the terms ΔI,IIβγ and Δβκ represent the547
non-homogeneous terms according to Table A.1. In addition, in eqs. (A.8b) and (A.8g), we548
have denoted the integral terms as follows549
Δβ =1
Vβ
∫Aβκ
nβκ ·[−ζβI+∇Zβ
]dA+
1
Vβ
∫Aβγ
nβγ ·[−ζβI+∇Zβ
]dA (A.9a)
Δγ =1
Vγ
∫Aβγ
nγβ ·[−ζγI+∇Zγ
]dA (A.9b)
The domain of solution of these closure problems are periodic unit cells that reasonably550
represent the complicated pore structure and the distribution of the dispersed phase. An551
example of a 2-D unit cell used in this work is sketched in Figure A.1; here we represent552
the κ-phase as a circle of radius rκ =√
(1− ε) /π. The radii of the circles representing the553
γ-phase, rγ1, · · · , rγ5 are related to each other as: rγi = λirγ1 (i = 2, · · · , 5) and554
rγ1 =√Sγε/
{π(4 + 4 (λ2)
2 + 8 (λ3)2 + 8 (λ4)
2 + 4 (λ5)2]} (A.10)
The values of λi, i = 2, · · · , 5 are provided in Table A.2 for each porosity used in this work.555
The position of these circles was chosen in a way that the assumptions of non-coalescence556
and no contact with the solid phase are met.557
To conclude this section, we analyze the expression of the effective-medium coefficients558
involved in the LEM, Eq. (26c) and Eq-(26d) in terms of the corresponding closure variables559
in order to obtain an equivalent definition that expresses the intrinsic permeability and the560
relative effect of the dispersed flow contributions. From the Table A.1 we can define the561
effective coefficients as follows562
20
εμβ (Ke)−1 = μβ
1
Vf
∫Aβκ
nβκ · [−aβI+∇Aβ] dA+ μβ1
Vf
∫Aβγ
nβγ · [−aβI+∇Aβ] dA
+ μγ1
Vf
∫Aβγ
nγβ · [−aγI+∇Aγ ] dA (A.11)
μβhe = μβ
1
Vf
∫Aβγ
nβγ · [−ϕβI+∇fβ] dA+ μγ1
Vf
∫Aβγ
nγβ · [−ϕγI+∇fγ] dA (A.12)
Using the boundary condition at the β−γ interface given by the Eq. (A.8d) under LME563
conditions, (i.e., ΔIIβγ = 0 and ΔII
βγ = 2Hσnβσ) we have564
μβ
[−aβI+(∇Aβ +∇AT
β
)] · nβγ = μγ
[−aγI+(∇Aγ +∇AT
γ
)] · nβγ
and565
μβ
[−ϕβI+(∇fβ +∇fTβ
)] · nβγ = μγ
[−ϕγI+(∇fγ +∇fTγ
)] · nβγ + 2Hσnβσ
Integrating these boundary conditions along the fluid-fluid interface and taking into566
account the solenoidal nature of the fields of the closure variables Aβ, Aγ, fβ and fγ , leads567
to the following identities568
μβ1
Vf
∫Aβγ
nβγ · [−aβI+∇Aβ] dA = −μγ1
Vf
∫Aβγ
nγβ · [−aγI+∇Aγ ] dA (A.13)
569
μβ1
Vf
∫Aβγ
nβγ · [−ϕβI+∇fβ] dA = −μγ1
Vf
∫Aβγ
nγβ · [−aγI +∇Aγ] dA (A.14)
Under these conditions, we may simplify eqs.(A.11) and (A.12) to570
−ε (Ke)−1 =1
Vf
∫Aβκ
nβκ · [−aβI+∇Aβ ] dA (A.15)
571
he = − 1
Vf
∫Aβγ
2HσnβγdA (A.16)
21
Appendix B. Constraints for the local mechanical equilibrium572
This part of the paper is dedicated to derive the length-scale constraints supporting the573
assumption of local mechanical equilibrium. As a first step towards this goal, let us use the574
macroscopic decomposition given by Eq. (24) and the definition of the intrinsic macroscopic575
properties expressed in Eq. (22) in order to obtain576
εβψβ = (εβ − ε)ψγ =εβ (ε− εβ)
ε
(〈ψβ〉β − 〈ψγ〉γ
)(B.1)
Certainly, for conditions in which(〈ψβ〉β − 〈ψγ〉γ
)= 0, it follows from the above result that577
the macroscopic deviations will be zero. However, this is rarely the case. In practice, the578
main assumption behind the local mechanical equilibrium is the following579
〈ψβ〉β ≈ 〈ψ〉 ≈ 〈ψγ〉γ , local mechanical equilibrium is valid (B.2)
From Eq. (25), we notice that, whenever the following assumptions are reasonable580
ε−1 (μβ − μγ)SβSγ∇2(〈vβ〉β − 〈vγ〉γ
)� 〈μ〉 (Ke)−1 · ε 〈v〉 (B.3a)
581 [(−μβSβKββ−1 + μγSγKγβ
−1)SβSγ + μβSβKβγ + μγSγKγγ
]·(〈vβ〉β − 〈vγ〉γ)� 〈μ〉 (Ke)−1·ε 〈v〉
(B.3b)582
(μβSβuβ + μγSγuγ) ·(〈pβ〉β − 〈pγ〉γ
)� 〈μ〉 (Ke)−1 · ε 〈v〉 (B.3c)
we can discard the Φ term in Eq. (25) and thus obtain an equilibrium model. An order of583
magnitude analysis in (B.3), gives rise to the following inequalities584
ε−1 (μβ − μγ)SβSγ
ε 〈μ〉 (Ke)−1Lv1Lv
(〈vβ〉β − 〈vγ〉γ
〈v〉
)� 1 (B.4a)
585 (−μβSβK−1ββ + μγSγK
−1γβ
)SβSγ + μβSβKβγ + μγSγKγγ
ε 〈μ〉 (Ke)−1
(〈vβ〉β − 〈vγ〉γ
〈v〉
)� 1 (B.4b)
586
(μβSβuβ + μγSγuγ)
ε 〈μ〉 (Ke)−1
(〈pβ〉β − 〈pγ〉γ
〈v〉
)� 1 (B.4c)
in which Kββ, Kγβ , Kβγ and Kγγ ,are the norms of Kββ, Kγβ, Kβγ and Kγγ respectively. In587
(B.4a) we have assumed that the length scales for ∇〈v〉 and 〈v〉 are Lv1 and Lv, respectively.588
From the above inequalities it is clear that it is necessary to have estimates of the differences589
〈vβ〉β − 〈vγ〉γ and 〈pβ〉β − 〈pγ〉γ in order to derive the length-scale constraints supporting590
the local mechanical equilibrium assumption. With this in mind, let us subtract Eq. (13)591
to Eq. (11) to obtain592
22
0 = −∇(〈pβ〉β − 〈pγ〉γ
)+ (ρβ − ργ)g + μβ∇2 〈vβ〉β − μγ∇2 〈vγ〉γ
+(μβεβ (−Kββ)
−1 − μγεγ (−Kγβ)−1) · 〈vβ〉β + (μβKβγ − μγKγγ) ·
(〈vβ〉β − 〈vγ〉γ
)+
(μβuβ − μγuγ)(〈pβ〉β − 〈pγ〉γ
)+ (μβhβ − μγhγ) (B.5)
At this point, it is convenient to notice that a proper combination of eqs. (B.1) and (24)593
leads to the following relation594
〈ψα〉α = 〈ψ〉+ ελε
(〈ψβ〉β − 〈ψγ〉γ
), α, λ = β, γ, α �= λ, ψ = v, p (B.6)
Substituting the above expression into Eq. (B.5) and after some algebraic manipulations595
we can eventually obtain596
∇(〈pβ〉β − 〈pγ〉γ
)μβγ
− eβγμβγ
(〈pβ〉β − 〈pγ〉γ
)−∇2
(〈vβ〉β − 〈vγ〉γ
)−
(SγCβγ +Dβγ) ·(〈vβ〉β − 〈vγ〉γ
)− (ρβ − ργ)
μβγg − hβγ =
(μβ − μγ)
μβγ∇2 〈v〉+ Cβγ · 〈v〉
(B.7)
Here, we introduced the following definitions597
μβγ = μβSγ − μγSβ (B.8a)
598
Cβγ =μβεβ (−Kββ)
−1 − μγεγ (−Kγβ)−1
μβγ(B.8b)
599
Dβγ =μβKβγ − μγKγγ
μβγ(B.8c)
600
eβγ = μβuβ − μγuγ (B.8d)601
hβγ = μβhβ − μγhγ (B.8e)
From Eq. (B.7), it can be demonstrated that, for cases in which the volumetric fraction of602
one phase is much larger than the other (for example, if εγ εβ) or if the properties of603
both fluid phases are equal, the local mechanical equilibrium assumption is automatically604
satisfied. However, we are interested in cases in which the above conditions may not be605
met. For this reason, in the following paragraphs we will perform an analysis of orders of606
magnitude in order to estimate the ratio(〈vβ〉β − 〈vγ〉γ
)/ 〈v〉. We begin our derivations by607
estimating the order of magnitude of each term on the left-hand side of Eq. (B.7)608
23
∇(〈pβ〉β − 〈pγ〉γ
)μβγ
= O
(〈pβ〉β − 〈pγ〉γ
μβγL
)(B.9a)
eβγμβγ
(〈pβ〉β − 〈pγ〉γ
)= O
(〈pβ〉β − 〈pγ〉γ
μβγ�
)(B.9b)
∇2(〈vβ〉β − 〈vγ〉γ
)= O
(〈vβ〉β − 〈vγ〉γ
L2
)(B.9c)
(SγCβγ +Dβγ) ·(〈vβ〉β − 〈vγ〉γ
)=⎧⎨
⎩O
⎡⎣Sγ
(〈pβ〉β − 〈pγ〉γ
)Lμβγ
⎤⎦+O
(1
�2
)⎫⎬⎭(〈vβ〉β − 〈vγ〉γ
)(B.9d)
−(ρβ − ργ) g
μβγ− hβγ = O
(〈pβ〉β − 〈pγ〉γ
μβγL
)(B.9e)
For the sake of simplicity, we have taken L to represent the characteristic length associated to609
the spatial variations of any volume-averaged quantity, whereas � denotes the characteristic610
length related to the changes of properties defined at the microscale. In addition, the order611
of magnitude for the tensor Cβγ was obtained from the definition given in Eq. (B.8b) and612
the NLME model (eqs. (11) and (13)). Assuming that the pressure gradient term and the613
term that includes the effective coefficients (−Kββ)−1 and (−Kγβ)
−1 are of the same order,614
we have615
O(−K−1
ββ
)= O
(∇〈pβ〉βμβεβ 〈vβ〉β
), O
(−K−1γβ
)= O
( ∇〈pγ〉γμβεβ 〈vγ〉γ
)(B.10)
Furthermore, for conditions in which the estimate O(〈vβ〉β
)= O (〈v〉) is reasonable, it616
follows that617
Cβγ = O
(〈pβ〉β − 〈pγ〉γLμβγ 〈v〉
)(B.11)
To advance in our derivations, it is convenient to write the complete expressions for Dβγ,
24
eβγ and hβγ in terms of the corresponding closure variables,
Dβγ =μβε
−1β
μβγ
⎛⎜⎝ 1
V
∫Aβκ
nβκ · [−aβγI+∇Aβγ ] dA+1
V
∫Aβγ
nβγ · [−aβγI+∇Aβγ] dA
⎞⎟⎠−
μγε−1γ
μβγ
⎛⎜⎝ 1
V
∫Aβγ
nγβ · [−aγβI+∇Aγβ] dA
⎞⎟⎠ (B.12a)
eβγ = μβε−1β
⎛⎜⎝ 1
V
∫Aβκ
nβκ · [−sβI+∇dβ] dA+1
V
∫Aβγ
nβγ · [−sβI+∇dβ ] dA
⎞⎟⎠−
μγε−1γ
⎛⎜⎝ 1
V
∫Aβγ
nγβ · [−sγI+∇dγ ] dA
⎞⎟⎠ (B.12b)
hβγ = μβε−1β
⎛⎜⎝ 1
V
∫Aβκ
nβκ · [−ϕβI +∇fβ] dA+1
V
∫Aβγ
nβγ · [−ϕβI+∇fβ ] dA
⎞⎟⎠−
μγε−1γ
⎛⎜⎝ 1
V
∫Aβγ
nγβ · [−ϕγI+∇fγ] dA
⎞⎟⎠ (B.12c)
Therefore, the order of magnitude estimates for Dβγ , eβγ and hβγ can be expressed as618
O (Dβγ) = O
[μβε
−1β
μβγ
1
�2,μγε
−1γ
μβγ
1
�2
](B.13a)
619
O (eβγ) = O
[μβε
−1β
1
μβ�, μγε
−1γ
1
μγ�
](B.13b)
620
O (hβγ) = O
[μβε
−1β
σ
μβ�2, μγε
−1γ
σ
μγ�2
](B.13c)
here, we have taken into account the derivations provided in Appendix A in order to write621
the following estimates622
Aβγ = O(1), Aγβ = O(1), aβγ = O
(1
�
), aγβ = O
(1
�
)(B.14a)
25
623
dβ = O
(�
μβ
), dβ = O
(�γμγ
)sβ = O
(1
μβ
), sγ = O
(1
μγ
)(B.14b)
624
fβ = O
(σ
μβ
), fβ = O
(σγμγ
)ϕβ = O
(σ
μβ�
), ϕγ = O
(σ
μγ�
)(B.14c)
We continue our derivations by examining the right-hand side of Eq. (B.7) and providing625
the estimate626
(μβ − μγ)
μβγ∇2 〈v〉 = O
(〈v〉L2
)(B.15a)
Cβγ · 〈v〉 = O
[(〈pβ〉β − 〈pγ〉γ
Lμβγ
)](B.15b)
On the other hand, we can estimate the pressure difference from eqs. (11) and (13) to obtain627
O(〈pβ〉β − 〈pγ〉γ
)= O
⎡⎣μβγ
(〈vβ〉β − 〈vγ〉γ
)�
⎤⎦ (B.16)
Substitution of the estimates for the left- and right-hand side of Eq. (B.7), gives rise,628
after some manipulation, to the following expression, which is applicable at the first order629
for〈vβ〉β−〈vγ〉γ
〈v〉 ,630
〈vβ〉β − 〈vγ〉γ〈v〉 = O
(�
L
)2{
1
1 +O(�L
)+O
(�L
)2}
(B.17)
here, the terms with the same order of magnitude have been collapsed into one term (eqs.631
B.9a, B.9e and B.15b). For simplicity, we have replaced Lv, Lv1 and Lp with L. Furthermore,632
under the assumption633
〈vβ〉β − 〈vγ〉γ〈v〉 � L
�(B.18)
and using the length scale constraint �� L we have634
〈vβ〉β − 〈vγ〉γ〈v〉 = O
(�
L
)2
� 1 (B.19)
which is the desired constraint for local mechanical equilibrium assumption to be valid.635
26
Nomenclature636
Aβγ continuous-dispersed phases interface, m2
Aβκ continuous-solid phase interface, m2
Aα closure variables tensors that map 〈vβ〉β onto vα
Aαλ closure variables tensors that map 〈vβ〉β − 〈vγ〉γ onto vα
aα closure variables vectors that map μα 〈vβ〉β onto pα, m−1
aαλ closure variables vectors that map μα
(〈vβ〉β − 〈vγ〉γ
)onto pα, m
−1
dα closure variables vectors that maps 〈pβ〉β − 〈pγ〉β onto vα, m s−1Pa−1
dp pore diameter in the unit cell (=(√
1/2)�c − 2rκ)
fα closure variables vectors that maps H onto vα, ms−1
g gravitational acceleration vector, ms−2
H mean curvature, m−1
hα effective vector, Pa m−1
he effective vector, Pa m−1
I unit tensorK Darcy’s permeability tensor, m2
Ke effective tensor, m2
Km effective tensorKne
αα effective tensor, (α = β, γ) m2
Kneαλ effective tensor, (α, λ = β, γ, α �= λ) m−2
�c width of the unit cell, m�α characteristic length for the α-phase, (α = β, γ) m�p small scale representation of the mean pore diameter, mL characteristic length associated with volume averaged quantities, mNγ number of circles needed to represent the dispersed γ-phase in the unit cellnβκ unit normal vector pointing from the β-phase towards the κ-phase.nβγ unit normal vector pointing from the β-phase towards the γ-phase (= nγβ)pα pressure in the α-phase, (α = β, γ), Pa〈pα〉 superficial averaged pressure in the α-phase, (α = β, γ) Pa〈pα〉α intrinsic averaged pressure in the α-phase, (α = β, γ), Papα pressure deviations in the α-phase, Papα non-equilibrium spatial deviations of pressure of the α-phase, Pa〈p〉 average pressure in the equilibrium, Par0 radius of the averaging volume V , mr position vector, m
rκ radius of the κ-phase in the unit cell (=√
(1− ε) /π), mrγ radius of the γ-phase in the unit cell, mSα saturation (= εα/ε, α = β, γ)
sα closure variable that maps μα
(〈pβ〉β − 〈pγ〉β
)onto vα, Pa s−1
t time, st∗ characteristic process time, s
637
27
uα effective vector, (Pa m s )−1
vα velocity vector in the α-phase, ms−1
〈vα〉 superficial averaged velocity in the α-phase, ms−1
〈vα〉α intrinsic average velocity in the α-phase, ms−1
vα velocity deviations in the α-phase, ms−1
vα local non-equilibrium spatial deviation velocity of α-phase, ms−1
〈v〉 average velocity in the equilibrium model, ms−1
Vα volume of the α-phase, contained within the averaging volume, m3
V averaging volume, m3
Vf (= Vβ + Vγ) fluid-phase volume in the averaging domain, m3
V magnitude of the averaging domain, m3
yα position vector that locates points in the α-phase relative to the centroid of V , m
638
Greek letters639
ε porosityεα volume fraction of the α-phaseμα viscosity of the α-phase, Pa · s〈μ〉 average viscosity, Pa · sρα density of α-phase, kg m−3
ν (= μβ/μγ) viscosity ratio〈ρ〉 average density, kg m−3
σ interfacial tension between the β- and γ-phase N/mϕα closure variable that maps μαH onto pαΦ non-equilibrium mechanical source,
640
Sub and superscripts641
β fluid continuous phaseγ fluid dispersed phaseκ solid phasene non-equilibrium modele equilibrium model
642
Acknowledgments643
This work was supported by Fondo Sectorial de Investigacion para la Educacion from644
CONACyT (Project number: 12511908; Arrangement number: 112087). OALR thanks645
CONACyT for the doctoral scholarship 274032. Both authors are grateful to Dr. Didier646
Lasseux, Dr. J. Alberto Ochoa-Tapia and M.in Sc. Raquel de los Santos for their valuable647
comments and suggestions.648
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30
Figures captions722
Fig. 1. Characteristic length scales and averaging volume.723
Fig. 2. Examples of the fields of the closure variables (Aβ)xx and (Aγ)xx under different724
conditions: (a) ε = 0.5, Sβ = 0.8, ν = 1, (b) ε = 0.5, Sβ = 0.8, ν = 0.1, (c) ε = 0.8,725
Sβ = 0.8, ν = 1 and (d) ε = 0.8, Sβ = 0.8, ν = 10726
Fig. 3. Predictions of the longitudinal component of the effective coefficient Ke for the LME727
model as a function of the void fraction ε taking Sβ = 0.35 (a, c) and 0.8 (b, d) for728
several values of the viscosities ratios, ν.729
Fig. 4. Predictions of the correction factor, Km as a function of the void fraction, ε, for730
several values of ν, taking Sβ = 0.8.731
Fig. 5. Fields of the closure variables (Aβ)xx and (Aγ)xx for the experimental parameters732
corresponding to experiment number 3 of Soo and Radke (1984).733
Fig. 6. a) Comparison of the experimental data reported by Soo and Radke (1984) and734
the predictions of the effective coefficient for the LME model, Ke with respect to the735
intrinsic permeability, K. b) Relative error percent between theory and experiments.736
Fig. 7. a) Comparison of the experimental data reported by Jain and Demond (2002) and737
the predictions of the effective coefficient for the LME model, Ke with respect to the738
intrinsic permeability, K. b) Relative error percent between theory and experiments.739
Fig. A.1. Representative unit cell for dispersed flow.740
Tables captions741
Table 1. Parameters used for predicting the experimental data.742
Table A.1. Closure variables and non-homogeneous terms for the associated boundary743
value problems.744
Table A.2. Values for geometry parameter λi745
31
L Average scale (mm to 10cm)
Macroscopic scale (1m to 100m)
r0
Microscopic scale (mm to �m)
�-phase ℓ�ℓβℓκ
�-phase
�-phase
Figure 1: Characteristic length scales and averaging volume.
1
Figure 2: Examples of the fields of the closure variables (Aβ)xx and (Aγ)xx under different conditions: (a)ε = 0.5, Sβ = 0.8, ν = 1, (b) ε = 0.5, Sβ = 0.8, ν = 0.1, (c) ε = 0.8, Sβ = 0.8, ν = 1 and (d) ε = 0.8,Sβ = 0.8, ν = 10
2
Figure 3: Predictions of the longitudinal component of the effective coefficient Ke for the LME model asa function of the void fraction ε taking Sβ = 0.35 (a, c) and 0.8 (b, d) for several values of the viscositiesratios, ν.
Figure 4: Predictions of the mixture coefficient, Km as a function of the void fraction, ε, for several valuesof ν, taking Sβ = 0.8.
3
Figure 5: Fields of the closure variables (Aβ)xx and (Aγ)xx for the experimental parameters correspondingto experiment number 3 of Soo and Radke (1984).
Figure 6: a) Comparison of the experimental data reported by Soo and Radke (1984) and the predictionsof the effective coefficient for the LME model, Ke with respect to the intrinsic permeability, K. b) Relativeerror percent between theory and experiments.
4
Figure 7: a) Comparison of the experimental data reported by Jain and Demond (2002) and the predictionsof the effective coefficient for the LME model, Ke with respect to the intrinsic permeability, K. b) Relativeerror percent between theory and experiments.
r�
�-phase
ℓcr�1r�3
r�4
r��
r�5
�-phase
�-phase
Figure A.1: Representative unit cell for disperse flow.
5
Table 1: Parameters used for predicting the experimental data.
Experiment number ε ν Sβ 2rγ [µm] dp [µm]Soo and Radke (1984)
1 0.34 0.660 0.16-0.1 3.1 29.52 0.34 0.660 0.20-0.7 6.1 29.53 0.34 0.044 0.01-0.06 3.4 29.5
Jain and Demond (2002)1 0.336 1.18 0.02-0.34 1.1 47
Table A.1: Closure variables and non-homogeneous terms for the associated boundary value problems.
Problem I Problem II Problem III Problem IV
Source: 〈vβ〉β 〈vβ〉β − 〈vγ〉γ 〈pβ〉β − 〈pγ〉β HClosure variables:Zα Aβ, Aγ Aβγ, Aγβ dβ, dγ fβ, fγζα aβ, aγ aβγ, aγβ sβ, sγ ϕβ, ϕγHomogeneous terms in α-phase:∆β −εβK−1
β Kβγ δβγ hβ∆γ −εγK−1
γ Kγβ δγβ hγNon-homogeneous terms at the interfaces∆βκ −I 0 0 0∆I
βγ 0 I 0 0∆II
βγ 0 0 +nβγ +2Hσnβγ
Table A.2: Values for geometry parameter λi
ε = 0.5 = 0.6 = 0.7 = 0.8 = 0.9λ2 0.55 0.55 0.55 0.75 1λ3 0.9 0.9 0.8 0.75 1λ4 0.62 0.62 0.65 0.5 0.95λ5 0.51 0.6 0.77 0.65 0.7
An upscaled model was derived to study two-‐phase dispersed flow in porous media A Darcy’s-‐law type model was obtained using a local mechanical equilibrium approach The effective-‐medium coefficient was sensitive to flow and geometrical parameters Good agreement was found with available experimental data
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